ML17286A327

Rev 1 to, BWR Transient Analysis Model.

ML17286A327
Person / Time
Site:	Columbia
Issue date:	09/30/1990
From:	LARKIN D L, VOSBURGH R O WASHINGTON PUBLIC POWER SUPPLY SYSTEM
To:
Shared Package
ML17286A326	List: ML17286A325 ML17286A327
References
WPPS-FTS-129-R01, WPPS-FTS-129-R1, WPPSS-FTS-129, NUDOCS 9010040216
Download: ML17286A327 (214)

Text

BWR TRANSIENT ANALYSIS MODEL WPPSS-FTS-129, Rev.01 September 1990 Principal Engineers Y.Y.YUNG S.H.BIAN D.E.BUSH Contributing Engineer B.M.Moore Approved: Date: R.O.Vosbur h Manager, Saf y'&Reliability Analysis Date: D.L.Larkin Manager, Engineering Analysis&Nuclear Fuel I I~~~

DIS CLAIMER This report was prepared by the Washington Public Power Supply System (" Supply System")for submittal to the Nuclear Regulatory Commission, NRC.The information contained herein is accurate to the best of the Supply System's knowledge.

The use of information contained in this document by anyone other than the Supply System, or the NRC is not authorized and with respect to any unauthorized use, neither the Supply System nor its officers, directors, agents, responsibility, or or employees assume any obligation, 0 liability or makes any warranty or representation concerning the contents of this document or its accuracy or completeness.

t 5~4 I 4;'tv ACKNOWLEDGEMENTS The Supply System acknowledges the consulting reviews and recommendations provided by Energy Incorporated and Yankee Atomic Electric Company during the course of development of this model.The Supply System also acknowledges the efforts of Mr.J.C.Chandler, Consultant, and Mr.Z..T.Cronin, Yankee Atomic Electric Company for their reviews and comments on this report.The technical discussions with Philadelphia Electric Company and Pennsylvania

'Power&Light Company regarding the Peach Bottom 0 benchmarks is greatly appreciated.

~~1 0*I l II ABSTRACT System-wide models, based on the WNP-2 plant-specific design and utilizing the RETRAN-02 computer code, are described.

Both best-estimate and conservative models are included.The models are applicable to a wide range of transients and will.initially be used for, but not limited to, analysis of the limiting pressurization transients considered for reload core licensing.

The best-estimate model is qualified by comparisons to a range of power ascension test transients and to the Peach Bottom Unit 2 Turbine Trip Tests.A representative application of the model for licensing basis calculations of the limiting pressurization transients (based on WNP-2 end of cycle 4 conditions) is also presented.

The benchmark comparisons show good agreement between calculated and measured data, thereby demonstrating the Supply System's capability to perform transient analyses for licensing applications.

l~l I TABLE OF CONTENTS Pacae

1.0 INTRODUCTION

....................1-1 2.0 MODEL DESCRIPTION 2-1 2.1 Model Geometry 2.1.1 Control Volumes, Junctions Conductors and Heat 2-6 2-6 2.1.2 Vessel Internals 2.1.3 Core Region 2.1.4 Recirculation Loops 2.1.5 Steam and Feedwater Lines 2.2 Component Models 2.2.1 Jet Pumps 2.2.2 Recirculation Pumps 2.2.3 Steam Separators 2,.2.4 Safety/Relief Valves 2.2.5 Core Hydraulics 2.3 Trip Logic 2.4 Control System Models 2.4.1 Feedwater Control System 2.4.2 Pressure Control System 2.4.3 Recirculation Flow Control System 2.4.4 Direct Bypass Heating 2.5 Steady-state Initialization 2-7 2'-8 2-9 2-10 2-16 2-16 2-17 2-17 2-18 2-19 2-21 2-23 2-23 2-24 2-25 2-25 2-35 TABLE OF CONTENTS (Continued)

2.6 RETRAN

Kinetics Pacae 2-35 2.6.1 2.6.2 2.6.3 2.6'General Description of the Generation of One-dimensional Data Calculation of the Initial Kinetic Input Data Adjustment of Kinetics Data Verification of the Supply System's Methodology 2-36 2-38 2-40 2-41 3.0 QUALIFICATION 3-1 3.1 WNP-2 Power Ascension Tests..'.*.......3-1 3~1~1 Water Level Setpoint Change (Test PAT 23A)3-4 3.1.1.1 RETRAN Model for Test PAT 23A.3-4 3.1.1.2 Results and Discussions

....3-4 3Pressure Regulator Setpoint Change (Test PAT 22)3-9 3.1.2.1 RETRAN Model for Test PAT 22.3-9 3.1.2.2 Results And Discussions

....3-9 3'3 One Recirculation Pump Trip (Test PAT 30A)3-15 3.1.3.1 RETRAN Model for Test PAT 30A.3-15 3.1.3.2 Results And Discussions

....3-16 3.1.4 Generator Load Rejection with Bypass (Test PAT 27)3-30 3.1.4.1 RETRAN Model for Test PAT 27.3-30 3.1.4.2 Results and Discussions

....3-31 TABLE OF CONTENTS (Continued)

3.2 Peach

Bottom Turbine Trip Tests Pacae 3-40 3.2.1 Test Description

............3-40 3.2.2 Peach Bottom Unit 2 Model Description

.3-42 3.2.3 Initial Conditions and Model Inputs..3-44 3.2.4 Comparison with Measurements

......3-47 3.2.4.1 Pressure Comparisons 3-47 3.2.4.2 Power and Reactivity Comparisons 3-62 4.0 LICENSING BASIS ANALYSIS 4.1 Licensing Basis Model 4.2 Load Rejection Without Bypass (LRNB)4.2.1 Sequence of Events 4.2.2 Results of LRNB RETRAN Analysis 4.3 Feedwater Controller Failure to Maximum (FWCF)~~~~~~~~~~~~~~~~4.3.1 Sequence of Events 4.3.2 Results of FWCF RETRAN Analysis 4.4 Summary of Transient Analysis Demand 4-1 4-2 4-8 4-8 4-10 4-27 4-27 4-28 4-53 5.0

SUMMARY

AND CONCLUSIONS

.....~.~......5-1

6.0 REFERENCES

............~~~......6-1 LIST OF FIGURES Ficiure 2.1 2.2 2.3 2.4 2 2 1 2.4.1 2;4.2 2.4.3 2.6.1 2.6.2 2.6.3 Supply System Reload Transient Analysis Methods Computer Flow Chart WNP-2 RETRAN Model (Vessel)WNP-2 RETRAN Model (Active Core Region)WNP-2 RETRAN Model (Recirculation Loops)WNP-2 RETRAN Model (Steam Line)Jet Pump Performance Curve Feedwater Control System Pressure Control System Direct Bypass Heating.Initial Axial Power Distribution Peach Bottom Unit 2 TT1 Initial Axial Power Distribution Peach Bottom Unit 2 TT2 Initial Axial Power Distribution Peach Bottom Unit 2 TZ3 Pacae 1-5 2-2 2-3 2-4 2-5 2-20 2-27 2-31 2-34 2-43 2-44 2-45 3.F 1 3.1;2 3.1.3 3.1.4 3.1.5 3.1.6 3 1 7 3.1.8 3.1.9 3.1.10 Feedwater Flow-PAT Test 023 Water Level-PAT Test 023 Dome Pressure-PAT Test 022 Normalized Power-PAT Test 022 Steam Flow-PAT Test 022 Feedwater Flow-PAT Test 022 Recirc Flow Pump A-PAT Test 030A Recirc Flow Pump B-PAT Test.030A Recirc Flow Pump A-PAT Test 030A Recirc Flow Pump B-PAT Test 030A 1D 1D 3-7 3-8 3-11 3-12 3-13 3-14 3-18 3-19 3-20 3-21 iv Ficiure 3.1.11 32 3.1.13 3.1.14 3.1.15 3.1.16 3.1.17 3.-1.18 3.1.19 3.1.20 3.1.21 3'.22 3.1.23 3.1.24 3~2 3 2~1 3.2.2 3.2.3 3.2.4 3.2'3.2.6 3.2.7 3.2.8 LIST OF FIGURES (Continued)

Jet Pump A Flow-PAT Test 030A Zet Pump B Flow-PAT Test 030A Zet Pump A Flow-PAT Test 030A-1D Zet Pump B Flow-PAT Test 030A-1D Power-PAT Test 030A Power-PAT Test 030A-1D RETRAN Core Heat Flux-PAT Test 030A'ore Heat Flux-PAT Test 030A Power-PAT Test 027 RRC Flow A-PAT Test 027 RRC Flow B-.PAT Test 027,.Total Core Flow-PAT Test 027 Dome Pressure-PAT Test 027 Steam Flow-PAT Test 027 PB2 RETRAN Model PB TT1 Turbine Inlet Pressure PB TT2 Turbine Inlet Pressure PB TT3 Turbine Inlet Pressure PB TT1 Steam Dome Pressure PB TT2 Steam Dome Pressure PB TT3 Steam Dome Pressure PB TT1 Upper Plenum Pressure PB TT2 Upper Plenum Pressure 1D~~Pacae 3-22 3-23 3-24 3-25 3-26 3-27 3-28 3-29 3-34 3-35 3-36 3-37 3-38 3-39 3.-43 3-50 3-51 3-52 3-53 3-54 3-55 3-56 3-57 LIST OF FIGURES (Continued)

Ficiure 3.2.9 3.2.10 PB TT3 Upper Plenum Pressure PB TTl Upper Plenum Pressure 3~2.12 3~2.13 3.2.14 3.2.15 3.2.16 3.2.17 3.2.18 3.2.19 3.2.20 31 32 33 3.2.24 3.2.25 3'.26 3.2 27 3.2.28 3.2.29 3'.30 4.2.1 PB TT3 Upper Plenum Pressure PB TT1 Core Average Power PB TT2 Core Average Power PB TT3 Core Average Power PB TTl Level A Average LPRM PB TTl Level B Average'LPRM;PB TTl Level C Average LPRM PB TT1 Level D Average LPRM PB TT2 Level A Average LPRM PB TT2 Level B Average LPRM PB TT2 Level C Average LPRM PB TT2 Level D Average LPRM.PB TT3 Lhvel A Average LPRM.PB TT3 Level B Average LPRM.PB TT3 Level C Average LPRM.PB TT3 Level D Average LPRM PB TT1 Reactivity PB TT2 Reactivity

.PB TT3 Reactivity WNP-2 LRNB LBM-Steamline Pressure 3.2.11 PB TT2 Upper Plenum Pressure Pacae 3-58 3-59 3-60 3-61 3-67 3-68 3-69 3-70 3-71 3-72 3-73 3-74 3-75 3-76 3-77 3-78 3-79 3-80 3-81 3-82 3-83 3-84 4-13 Vi LIST OF FIGURES (Continued)

Ficiure 4.2.2 4.2.3 4.2.4 4.2.5 4.2.6 4.2.7 4.2'44.2.10 4.2.11 4.2.12 4.2.13 4.2.14 4~3~1 4.3.2 4.3.3 4.3.4 4'.5 4.3.6 44.3'4'.9 4.3.10 WNP-2 LRNB LBM-Vessel Steam Flow WNP-2 LRNB LBM-Dome Pressure A WNP-2 LRNB LBM-Pressure (Mid-Core)

WNP-2 LRNB LBM-Pressure (Core Exit)WNP-2 LRNB LBM-Total Reactivity

.WNP-2 LRNB LBM-Core Power WNP-2 LRNB LBM-Core Average Heat Flux WNP-2 LRNB LBM-Liquid Level WNP-2 LRNB LBM-Feedwater Flow WNP-2 LRNB LBM-Void Fraction (Mid-Core)

WNP-2 LRNB LBM-Void Fraction (Core Exit)WNP-2 LRNB LBM-Recirculation Flow WNP-2 LRNB LBM-Core Inlet Flow WNP-2 FWCF LBM-Feedwater Flow.WNP-2 FWCF LBM-Core Inlet Subcooling WNP-2 FWCF LBM-Liquid Level WNP-2 FWCF LBM-Turbine Steam Flow.WNP-2 FWCF LBM-Turbine Bypass Flow WNP-2 FWCF LBM-Dome Pressure WNP-2 FWCF LBM-Total Reactivity WNP-2 FWCF LBM-Core Power WNP-2 FWCF LBM-Core Average Heat Flux WNP-2 FWCF LBM-Group 1 SRV Flow Pacae 4-14 4-15 4-16 4-17 4-18 4-19 4-20 4-21 4-22 4-23 4-24 4-25 4-26 4-31 4-32 4-33 4-34 4-35 4-36 4-37 4-38 4-39 4-40 vii LIST OF FIGURES (Continued)

I Ficiure 4.3.11 4.3.12 4.3.13 4.3.14 4.3.15 4.3.16 4.3.17 4.3.18 4.3.19 4.3.20 4.3.21 4.3.22 WNP-2 FWCF LBM WNP-2 FWCF LBM WNP-2 FWCF LBM WNP-2 FWCF LBM Group 2 SRV Flow Group 3 SRV Flow.Group 4 SRV Flow Group 5 SRV Flow WNP-2 FWCF LBM WNP-2 FWCF LBM WNP-2 FWCF LBM WNP-2 FWCF LBM WNP-2 FWCF LBM WNP-2 FWCF LBM WNP-2 FWCF LBM Core Inlet Flow Core Exit Flow Recirculation Flow Pressure (Mid-Core)

Pressure (Core Exit)Void Fraction (Mid-Core)

Void Fraction (Core Exit)WNP-2 FWCF LBM-Vessel Steam Flow~~Pacae 4-41 4-42 4-43 4-44 4-45 4-46 4-47 4-48 4-49 4-50 4-51 4-52 LIST'OF TABLES Table 2.1.1 2~1~2 2~1~3 2.3.1 2.4.1 3~2~1 Description of Trip Logic Control Input Definition Peach Bottom Turbine Trip Tests Test Conditions 2-22 2-26 3-41 Pacae Volume Geometric Data.............2-12 Junction Geometric Data............2-13 Heat Conductor Geometric Data.........2-15 3Peach Bottom Turbine Trip Tests Initial Conditions 3-46 3.2'Peach Bottom Turbine Trip Tests Pressure change (Psi)at Peak of First Oscillation 3-49 3.2.4 3.2.5 Peach Bottom Turbine Trip Tests Summary of Core Average Peak Neutron Power..Peach Bottom Turbine Trip Tests Time (Sec)of Peak Neutron Power 3-64 3-64 3.2.6 Peach Bottom Turbine Trip Tests Summary of LPRM Level Neutron Power Peaks 3-65 3'.7 4.1 4.2 Peach Bottom Turbine Trip Tests Reactivity Summary Input Parameters and Initial Transient Conditions, Comparison of Licensing Basis and Nominal plant Conditions Technical Specification Limits Maximum Control Rod Insertion Time to Position'fter Deenergization of Pilot Valve Solenoids 3-66 4-3 4-6 4.3 Sequence of Events for LRNB Transient 4-9 4'4.5 Sequence of Events for Feedwater Controller Failure t~~~~~~~~~~~~~~~~~~~Summary of Pre'ssurization Transient Results 4-30 4-53 ix l'g~l I

1.0 INTRODUCTION

This report describes and presents qualification results of a transient analysis model for WNP-2.WNP-2 is a boiling water reactor using a BWR/5 Nuclear Steam Supply System (NSSS)provided by General Electric (GE)and operated by the Washington Public Power Supply System (The Supply System).The transient, analysis model, developed by the Supply System, uses the RETRAN-02 MOD04 ("RETRAN-02" or"RETRAN")computer code.As demonstrated in this topical report, the transient analysis model shows good agreement to operational transients using plant data and with proper input assumptions gives limiting or conservative results applicable to core reload or licensing analyses.RETRAN-02 is a versatile time dependent computer code developed by the Electric Power Research Institute (EPRI)to model complex thermal-hydraulic systems.It is capable of providing realistic responses to system upset conditions.

A user inputs a system model consisting of control volumes, heat slabs, and a flow path network;for nuclear reactor systems a kinetics model utilizing either point or one-dimensional kinetics is available.

The RETRAN-02 computer code was developed by utility sponsorship through EPRI.The computer code qualification studies were based on code predictions of various separate effects tests, system effects experiments, and power reactor startup tests which can be 1-1 found in the RETRAN-02 documentation.

The NRC Staff's'Safety Evaluation Report (SER)for RETRAN-02 has been issued.The NRC found"...RETRAN-02 is an acceptable computer program for use in licensing applications for calculating the transients described in Chapter 15...and other transients and events as appropriate and necessary for nuclear power plant operation.".

The RETRAN-02 limitations discussed in the SER and applicable to reload licensing analysis will be addressed in the Supply System Applications Topical Report (to be submitted later).The Supply System has developed the input for the model presented in this report, representing the WNP-2 plant, from as-built drawings and vendor specifications.

The nodalization network was developed over many years by trial and error, comparison to similar plant models, and finally through comparison of model predictions to actual WNP-2 data.This report provides qualification of the WNP-2 RETRAN model and of the Supply System's ability to analyze WNP-2 transient behavior through the application of RETRAN-02 to the analysis of 1.WNP-2 Power Ascension Tests;2.Peach Bottom 2 Cycle 2 Turbine Trip Tests;and 3.WNP-2 Licensing Basis Analysis.The Supply System's reload transient analysis methods are based on the EPRX code package as depicted in Figure 1.1.The steady 1-2 state core physics.codes and models used to provide input to the transient analysis models are described and qualified elsewhere.The SIMTRAN-E MOD3A ("SIMTRAN-E")

code collapses the three-dimensional neutronics data generated by the steady state core physics codes to the one-dimensional neutronics input required by RETRAN-02 and calculates the moderator density and fuel temperature dependencies.

The one-dimensional kinetics parameter dependencies generated by SIMTRAN-E are modified as described in Section 2.6 to account for differences between the RETRAN-02 one-dimensional and SIMULATE-E three-dimensional moderator'density calculations.

RETRAN-02 is used to model the NSSS and the VIPRE-01 MOD02 ("VIPRE-01")

code is used to model a single fuel assembly for thermal margin evaluations.

Thermal margin evaluation for WNP-2 is described and qualified in a separate Applications Topical Report (to be submitted later).The base WNP-2 RETRAN-02 model is described in Chapter 2.It is designed to serve as a best-estimate, time dependent (transient), systems analysis tool.Intended uses of the best-estimate model include simulator qualification, evaluating operational transients, and evaluating proposed system design changes.In Chapter 3, the WNP-2 RETRAN-02 model is qualified by comparison of best-estimate data predictions with plant data collected during startup testing.To analyze limiting transients for core reload design in support of technical specification action, a Licensing Basis Model is developed by modifying the best estimate 1-3 model with conservative assumptions.

The Licensing Basis Model is described in Chapter 4, which also contains example calculations with the conservative model.The Applications Topical Report that will be published later will provide additional detail on a)the process and interface between the EPRZ codes for licensing analyses, b)the Licensing Basis Model input sensitivity and uncertainity analyses, and c)the hot channel thermal margin methodology.

Chapter 5 contains the Summary and Conclusions and Chapter 6 the References.

(1-4 FlGURE 1.1 Supply System Reload Transient Analysis Methods Computer Code Flow Chart CORE PHYSICS ANALYSIS SIMTRAN-E 3-0 to IN Link MODIFICATION OF CROSS SECTION DEPENDENCIES RETRAN-02 NSSS Model VIPRE-01 Mot Bundle Model 1-5 I I L i I l I

2.0 MODEL

DESCRIPTION This chapter describes the WNP-2 RETRAN-02 Best Estimate Model developed to analyze a wide range of transients.

The Supply System has been involved with the RETRAN development effort since 1979 and the WNP-2 model has evolved over time with our code development involvement.

In addition, the Supply System has had two separate and independent reviews performed on the WNP-2 model, by Energy Incorporated (now a Division of NUS Corp)and by Yankee Atomic.These reviews have provided valuable insights into the model and options used and are documented as part of the model development file.The best estimate model description is given in the following sections.Figures 2.1 through 2.4 depict the nodalization scheme utilized for the WNP-2 model, whereas Section 2.1 provides additional detail on the Model Geometry, Section 2.2 discusses models of special components such as the jet pumps and the safety relief valves, and the trip logic and control systems models are described in Sections 2.3 and 2.4, respectively.

The steady-state initialization is discussed in Section 2.5.The WNP-2 model uses twelve active core nodes as is shown in Figure 2.2 and the interface/input between the RETRAN WNP-2 model and the reactor physics input to the kinetics model is given in Section 2.6.2-1 FIGURE 2.1 WNP-2 RETRAN HODEL (Vessel)Q5 318 28 ga Qs pi~Qs 287 Q9 21 12 (y 18 22 2H Qi 0" 281 288 03 2-2 FIGURE 2'WNP-2 RETRAN MODEL (Active Core Region)CORE OUTLET 62 Qii 61 0 Qsi Is 9 59 58 Qss Qss Qs Qs Junction No.8 7 58 Q92 Qs Heutronlc Region Na 8 55 Qss 5 53 Qss Qs~liia, 0 2 51 0 CORE INLET Qi 2-3 s s IS a~00~~i~~i!Ofi~~~W To Turbine WNP-2 RETRAN MODEL (Steam Line)398 Stop 388 Valve Q378 Met well Safety Relief Valves 381 382 383 38'1 385 Q3ie 328 O326 Reactor Vessel 0363 338 368 358 361 358 Inboar d MSIV Bypass Line

2.1 Model'Geometry

The physical geometry and volume of the WNP-2 nuclear steam supply system is modeled as series of control volumes and junctions.

The following sections discuss this physical arrangement and how it is modeled in the WNP-2 RETRAN model.2.1.1 Control volumes, Junctions, and Heat Conductors The control volume nodes are defined as distinct regions within the primary system, such as the steam dome or downcomer,'s shown in Figures 2.1 through 2.4.The physical dimensions of the volumes, junction areas, lengths, etc.were obtained from WNP-2 plant specific as-built drawings.The nodalization scheme used has been developed over several years and is based on code limitations, solution stability, economical run-times, and, most importantly, agreement to experimental or test data.In Figures 2.1 through 2.4, the nodal volumes are denoted by numbers in small circles.The pertinent data associated with each of these volumes is given in Table 2.1.1.The mass/energy transfer between volumes is through junctions, depicted in Figures 2.1 through 2.4 as numbered arrows.The junction input data is given in Table 2.1.2.In Figure 2.2, the heat conduction in the active core region is shown as small squares numbered 1 2-6 through 12 for each active core volume.The pertinent data for each heat conductor is given in Table 2.1.3.Additional discussion of the salient nodalization by region is given in, Subsections

2.1.2 through

2.1.5 below.Features of WNP-2 that are represented by special control volumes, e.g., safety/relief valves, are discussed in Section 2.2.2.1.2 Vessel Internals (Refer to Figure 2.1)Volumes 18, 19, and 20 constitute the middle, lower, and upper downcomer regions, respectively, of the reactor vessel.The middle downcomer region, Vol.18, is the volume in which the feedwater and the saturated liquid and steam carryunder from the steam separators are mixed.The upper downcomer region, Vol.20, models the liquid/steam interface region and utilizes the RETRAN"non-equilibrium" option.This option is used in this volume to accurately account'or the superheating of steam during pressurization transients (the pressurization/de-pressurization effects are governed by this interface region).As shown in Figure 2.1, the steam dome, Vol.16, and the fluid region below the core support plate (lower plenum), Vol.3, are single large volumes.The jet pump volumes, Vol.1 and 2, are discussed further in Section 2.2.4.2-7 The upper plenum region above the upper guide plate, Vol.13, and the standpipes, Vol.14, are both modeled as single volumes.A single volume, Vol.15, is used to model the internal region of the 225 steam separators.

From the steam separator internal region, the major steam flow is to the steam dome, Vol.16, whereas the steam carryunder flows to and mixes in the middle downcomer, Vol.18, as mentioned above.2.1.3 Core Region (Refer to Figure 2.2).The WNP-2 core region is considered to be the twelve control volumes used to model the active region of the core (Vols.51 through 62), the single volumes for the unheated core inlet and outlet regions (Vols.4 and 11), and the core bypass single volume region.(The core bypass volume is shown on Figure 2.1 as Vol.12).There are two means of energy deposition modeled in the core region.In the active core volumes, twelve heat conductors are used to represent the reactor fuel.The geometric data for the heat conductors is presented in Table 2.1.3.In addition,'a direct moderator heating model is included to account for direct energy deposition into the active core volumes due to'amma and neutron heating.For the core bypass volume, a constant fraction of the core thermal power is directly deposited via a RETRAN non-conducting heat exchanger model.2-8 As shown in Figure 2.2, the one-dimensional kinetics calculations are supported by twenty-seven neutronic regions, i.e., twenty-five in the active core volumes and one per reflector volume.Thermal-hydraulic feedback of each active core and reflector volume is provided to the associated neutronic regions.This feedback of the calculated water density of each active core and reflector volume and the attendant corrections are discussed further in Section 2.6 of this report.The fuel temperature feedback for each'egion is provided by the heat conductor models in each active core volume.The average fuel rod is xepresented by three cylindrical regions-fuel, gap, and cladding.The cladding is modeled with four nodes, the gap one node, and the fuel region is modeled with six nodes.The material conductivity and heat capacity for the U02 fuel and the Zircaloy cladding are taken from MATPRO and WREM data.For purposes of the model benchmarking, the gap conductance of the average core region is assumed to be a constant value 2.1.4 Recirculation Loops (Refer to Figure 2.3)The two recirculation loops are modeled separately.

In each recirculation loop, five control volumes are used to represent the recirculation pump and loop piping.In each loop, a single volume is used to model ten jet pumps driven by the recirculation 2-9 loop.A special two-stream momentum mixing option is used by RETRAN to describe the interaction of the recirculation loop drive flow with the suction flow from the downcomer.

Additional detail of the jet pump and the recirculation pump modeling is provided in Section 2.2.2.1.5 Steam and Feedwater Lines (Refer to Figure 2.4)The four main steam lines are lumped into one composite line, which is divided into seven control volumes (see Figure 2.4).From the reactor vessel there are three volumes modeling the steam lines to the Main Steam Isolation Valves (MSIVs), Vols.310, 320, and 330.The middle of these volumes (Vol.320)is connected to the junctions representing the safety/relief valves.Due to their redundancy, the MSIVs are modeled as a single valve.The steam lines from the MSIVs to the turbine stop valves are also modeled in three volumes, Vols.340, 350, and 360.The middle of these volumes, Vol.350, provides a line model for the turbine bypass, whereas the third volume, Vol.360 provides the pressure feedback signal to the Pressure Control System.The steam line volume between the turbine stop valve and the turbine control valves is modeled as Vol.390.The flows from steam line to the turbine (through Zct.390)and, subsequently, to the condenser (through Zct.361)are modeled as 2-10 negative fill junctions with flow rates controlled by the Pressure Control System (see Section 2.4.2).The feedwater lines are modeled as a positive fill junction with flow rate controlled by the Feedwater Control System.For simulation of very fast transients, the feedwater is constant and explicit modeling of the lines and pumps is not necessary.

2-11 TABLE 2.1.1 VOLUME GEOMETRIC DATA FIOW HYDRAULIC AREA DIAMEKR FT2 (FF ELEV.(FF)1 2 3 4 11 12 13 14 15 16 18 19 20 51" 52 53 54 55 56 57 58 59 60 61 62 201 202 204 205 206 207 208 210 211 212 310 320 330 340 350 360 370 390 136.942 136.942 2240.000 66.640 111.280 950.708.943,000 400.000 442.834 6285.300 2196.700 2498.700 1901.700 83.955 83.955 83.955 83.955 83.955 83.955 83.955 83.955 83.955 83.955 83.955 125.933 148.000 30.500 115.000 43.500 91.710 148.000 30.500 115.000 43.500 91.710 446.430 275.370 555.400 504.280 2747.160 1654.540 2.56E+5 86.750 16.517 16.517 17.281 0.745 1.198 14.443 3,816-8.918 6.167 18.544 10.221 24.177 7.812 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.500 34.682 3.375 21.979 1.193 20.116 34.682 3.375 21.979 1.193 20.116 33.509 2.200 39.090 7.146 6.861 25.882 42.610 2.350 16.517 16.517 21.450 0.745 1.198 14.443 3.816 8.918 7.092 21.100 8.531 9.960 7.812 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.000 1.500 58.360 12.027 45.347 9.727 25.980 58.360 12.027 45.347 9.727 25.980 37.490 23.125 46.641 42.348 170.589 102,741 42.610 10.001 19.897 19.897 114.280 89.474 83.955 65.825 247,120 44.853 71.807 270.000 257.496 103.350 149.621 83.955 83.955 83.955 83.955 83.955 83.955 83.955 83.955 83.955 83.955 83.955 83.955 2.536 2.536 2.536 2.236 3.530 2.536 2.536 2.536 2.236 3.530 11.908 11.908 11.908 11.908 16.104 16.104 4520.000 8.674 1.592 1.592 0.781 0.045 0.045 0.182 17.738 0.505 0.641 20.768 2.256 2.162 0.732 0.045 0.045 0.045 0.045 0.045 0.045 0.045 0.045 0.045 0.045 0.045 0.045 1.797 1.797 1.797 1.193 0.948 1.797 1.797 1.797 1.193 0.948 1.947 1.947 1.947 1.947 2.264 2.264 75.862 2.350 9.917 9.917 0.000 17.281 30.526 17.281 31.724 35.540 44.458 50.615 34.302 10.125 42.823 18.026 19.026 20.026 21.026 22.026 23.026 24.026 25.026 26.026 27.026 28.026 29.026-19.409-16.510-15.492 6.487 7.680-19.409-16.510-15.492 6.487 7.680 21.464 21.206-15.930-21.792-28.650-40.903 21.460-16.196 JEF PUMP JEP PUMP IlNER PIZKi'1 (DRE INLET (DRE EKIT ONE BYPASS UPPER PLBRM STANDPIPE SEPARATOR MID DOWNCOMER IQWER DOWNCOtKR UPPER DOWNKMER (DRE 51 KORE 52 KjRE 53 (DRE 54 CORE 55 (DRE 56 GSE 57 CORE 58 CORE 59 GNE 510 (DRE 511 GNE 512 RRC 51 SUCFION RRC 51 PUMP RRC 51 HEADER INLET RRC 51 HEADER RRC 51 RISER RRC 52 SUCFION RRC 02 PUMP RRC 52 HEADER INIET RRC 52 HEADER RRC 52 RISER SKAM QlflZF STEAM LINE SKAM LINE STEAM LINE SKAM LINE (QVI3INMEÃF STEAM LINE 2-12 TABLE 2.1.2 JUNCTION GEOMETRIC DATA KtmECIS FUN JCl'.VOUJME AREA NO.FROM'Io FF2 I ELEV.FT HYDRAULIC L0SS DIAtEFER KEF.FF I 2 3 4 10 11 12 13 14 15 16 17 18 19 20 21 22 23 51 52 53 54 55 56 57 58 59 60 61 201 202 204 205 206 207 208 209 211 212 213 214 310 320 I 3 2 3 3 4 4 51 62 11 11 13 12 13 13 14 14 15 15 16 19.8970 19.8970 22.6680 54.1390 63.0464 83.9550 55.9920 45.1400 33.7960 30.6800 15 18 51 52 52 53 53 54 54 55 55 56 56 57 57 58 58 59 59 60 60 61 61 62 19 201 201 202 202 204 204 205 205 206 206 I 19 207 207 208 208 210 210 211 211 212 212 2 16 310 310 320 51.8250 83.9550 83.9550 83.9550 83.9550 83.9550 83.9550 83.9550 83.9550 83.9550 83.9550 83.9550 2.5360 2.5360 1.7924 2.5360 3.5300 0.4609 2.5360 2.5360 1.7924 2.5360 3.5300 0.4609 11.9080 11.9080 20 16 239.3200 20 18 149.6210 18 19 85.1340 4 12 1.5000 3 12 0.8420 19 I 1.7730 19 2 1.7730 9.9170 9.9170 17.2813 18.0261 30.5261 31.7240 31.7240 35.5400 44.4580 50.6250 50.6250 42.8330 34.3020 17.2813 17.2813 26.4340 26.4340 44.5030 19.0261 20.0261 21.0261 22.0261 23.0261 24.0261 25.0261 26.0261 27.0261 28.0261 29.0261 14.3750-16.5100-15.4920 6.4870 7.6800 26.4340 14.3750-16.5100-15'920 6.4870 7.6800 26.4340 54.0000 22.4300 0.5089 0.5089 0.0980 0.0101 0.0161.0.0149 0.1174 0.1071 0.4390 0.0885 0.0652 0.0427 0.0648 0.1139 0.2036 4.7330 4.7330 0.0659 0.0119 0.0119 0.0119 0.0119 0.0119 0.0119 0.0119 0.0119 0.0119 0.0119 0.0149 11.5544 13.8775 11.3119 11.1157 5.8550 3.8530 11.5544 13.8775 11.3119 11.1157 5.8550 3.8530 1.6132 2.5451 1.8300 1.8300-1.0000 3.2690 0.4117 0.7300 0.6800 0.4100-1.0000-1.0000 0.1800 0.2700-1.0000 6.9851 0.0542 0.0542 4.0100 0.0000 1.2400 1.2400 0.0000 1,2400 0.0000 1.2400 1.2400 0.0000 1.2400 1.2400 0.2450 0.6300-1.0000 0.5460 1.2860 0.2122 0.2450 0.6300-1.0000 0.5460 1.2860 0.2122 0.2721 0.3391 1.5920 1.5920 0.1960 0.0270 0.0319 0.0446 0.3022 0.5054 0.1569 0.4167 0.0518 0.7320 2.7500 0.0028 0.0019 0.2100 0.2100 0.0895 0,0446 0.0446 0.0446 0.0446 0.0446 0.0446 0.0446 0.0446 0.0446 0.0446 0.0446 1.7969 1.7969 1.7969 1.7969 0.9480 0.1083 1.7969 1.7969 1.7969 1.7969 0.9480 0.1083 1.9470 1.9470 JEF PUMP¹I DIKH JEF PUMP¹2 DISCH GNE MZF GNE¹I MZF KRE¹12 EXIT GNE OmfZF BYPASS OUI1ZF SFANDPIPE MZF SEPARATOR INLEF SEPARA'IOR QJFLZF IlNER DOME MZF MID DOWNGNER'INLET IVER DOWNKMER INLEF KRE BYPASS MZF¹2 KRE BYPASS INLEF¹1 JEF PUMP¹I SUCFION JEF PUMP¹2 SUCFION SEP.m MID IXMKMER KRE¹I EXIT GNE¹2 EXIT GNE¹3 EXIT KRE¹4 EXIT KRE¹5 EXIT KRE¹6 EXIT GNE¹7 EXIT GNE¹8 EXIT GNE¹9 EGT KRE¹10 EXIT GNE¹11 EXIT RRC LOOP¹I RRC LOOP¹1 RRC LOOP¹I RRC UDP¹I RRC IQOP¹I RRC 10OP¹I RRC lOOP¹2 RRC LOOP¹2 RRC KOP¹2 RRC lOOP¹2 RRC LOOP¹2 RRC rmP¹2 SKAM UNE SFEAM LINE 2-13 TABLE 2.1.2 (CONT.)JUNCTION GEOMETRIC DATA 65NECFS FIOW JCF.VOIHME AREA NO.FRCN m FF2 HYDRAULIC EIZV.INDIA IOSS DIAM EKR FF 1 FF COEF.FF DESCRIPFICN 330 320 330 3.6370 340 330 340 4.1250 350 340 350.16.1040 360 350 360 16.1040 380 360 390 14.1860 381 320 370 0.2238 382 320 370 0.4477 3&3 320 370 0.4477 384 320 370 0,4477 385 320 370 0.4477 602 0 13 1.0000 601 0 16 1.0000 490 0 18 5.0000 390 0 390 1.0000.361 0 350 1.0000 22.1800-15.1300-21.7920-27.5200-15.0210 21.4600 21.4600 21.4600 21.4600 21.4600 31.7240 69.1580 41.1000-16.1960-28.6500 2.9294 3.7365 7.0746 8.4864 3.7664 0.9757 0.9757 0.9757 0.9757 0.9757 0.0077 0.0391 0.0166 0.5765 5.2965 0.1852 0.1541 0.4203 1.1780 2.5762 0.2630 0.2630 0.2630 0.2630 0.2630 0.0000 0.0000 0.0000-1.0000-1.0000 1.0760 1.1460 1.9470 2.2640 2.1250 0.3775 0.3775 0.3775 0.3775 0.3775 1.1284 1.1284 0.1333 1.1280 1.3440 SKAM UNE SKAM LXNE SKAM LINE SKAM IZK SKAM ICE SRV INIEF SRV INIZP SRV INLEF SRV INLEF SRV INLEF HPCS RCIC LINE FEEDWATER LINE'IURBINE NHG FILL SKAM BYP KEG FILL 2-14 TABLE 2.1.3 HEAT CONDUCTOR GEOMETRIC DATA.HEAT M)IHME CN: 65DUCIOR SURFACE AREA (DtD.LEFT RIGHI'EM EIRY VOIlME LEFT RIGIII'O.INSIDE QJFSIDE)TYPE NO.(FT3 FT2 FT2)DESCRIPTION 1 2 3 4 5 6 7 8 9 10 11 12 51 52 53 54 55 56 57 58 59 60 61 62 CYL.1 CYL 1 CYL.1 CYL.1 CYL.1 CYL 1 CYL.1 CYL.1 CYL.1 CYL 1 CYL.1 CYL.1 60.27 60.27 60.27 60.27 60.27 60.27 60.27 60.27 60.27 60.27 60.27 60.27 0.0.0.0.0.0.0.0.0.0.0.0.5990.5990.5990.5990.5990.5990.5990.5990.5990.5990.5990.5990.CORE 1 GNE 2 GNE 3 GNE 4 GNE 5 (ORE 6 GNE 7 GNE 8 G)RE 9.GNE 10 (DRE 11 GNE 12.2-15

2.2 Component

Models The transient behavior of a BWR is affected by system components such as jet pumps, recirculation pumps and steam separators.

The following sections describe the major component models of the WNP-2 RETRAN model.2.2.1 Jet Pumps There are ten jet pumps in each of the two recirculation loops.The ten jet pumps per loop are modeled as a single jet pump.This jet pump is modeled as a single control volume in the WNP-2 RETRAN model.Jet pump performance is represented by a M-N characteristic curve (N as a function of M, M=The ratio of the suction flow to the driving flow, N=The ratio of the specific energy increase of the suction flow to the specific energy decrease of the driving flow).To determine RETRAN input parameters that produce the expected M-N characteristic curve for the WNP-2 jet pump, a RETRAN sub-model of the recirculation loop and jet pumps was set up.Pressure distribution data from the vendor was used to determine the suction and drive nozzle loss coefficients.

The momentum mixing formulation was applied to the suction and nozzle junctions.

All other junction and volume geometry data were calculated using design drawings.The M-N curve generated with this model is compared to vendor's data in 2-16 Figure 2.2.1.The comparison shows that this modeling technique provides an acceptable representation for the WNP-2 jet pumps.2.2.2 Recirculation Pumps The centrifugal pump model in RETRAN is used to represent the WNP-2 recirculation pumps.The pump unique characteristics (i.e., moment of inertia, rated values for pump flow, head and torque)and the pump homologous curves supplied to the RETRAN pump model are based on pump manufacturer's'ata

.Since the recirculation flow control is achieved by varying the position of the flow control valve, not by varying the pump speed, the recirculation pump motor is modeled with a constant speed.2.2.3 Steam Separators The steam separators couple the reactor core and the steam dome.I'he emphasis in modeling the separators is on achieving the appropriate coupling between these regions.The 225 steam separators are modeled as a single control volume.The Bubble Rise model in RETRAN is used to simulate the separator performance.

Referring to Figure 2.1, the interior of the separators is represented by Volume 15.The entering two-phase fluid flow is represented by Junction 14.Separation takes place 2-17 within Volume 15.The exiting steam and liquid flows are represented by Junction 15 and Junction 23 respectively.

The most important separator input parameters relative to the coupling between the reactor core and steam dome are the separator inlet inertia and the pressure drop across the separators.

The separator inertia is determined from vendor's data.It is calculated as a function of the separator inlet quality at the transient initial condition.

The separator inlet and exit loss coeffic'ients are determined by RETRAN using the steady state initialization option.The pressure drop distribution at the rated operating condition is in agreement with vendor's calculation 2.2.4 Safety/Relief Valves WNP-2 has 18 relief valves arranged in groups of 2 to 4 valves at a common setpoint.Each of the groups of valves at a common setpoint is represented by a junction connecting the steam line to a sink volume in the RETRAN model.The area of the junctions is taken as the flow area of the valve times the number of valves being modeled.When the valve is opened with the steam line pressurized, the junction flow becomes choked and the Moody critical flow option is chosen in RETRAN to calculate the choked flow rate.Contraction coefficients of the relief valve junctions 2-18 are adjusted to match the specified flow at the reference pressure.The opening and closing of the relief valves is modeled using RETRAN trips.When the pressure in the steam line volume containing the relief valves reaches the specified setpoint , the valve is opened linearly after a time delay.The valve stays fully open until the pressure drops to the reclosing setpoint.It is then completely closed in a stepwise manner.2.2.5 Core Hydraulic The core region is modeled using the compressible, single-stream flow with momentum flux form of flow equation.The two-phase friction multiplier is computed with the Baroczy correlation.

The form loss coefficients are set to match values calculated with a steady-state thermal-hydraulic model.This model was developed with the FIBWR code and has been benchmarked against plant data.Initial values of core bypass flow and core support plate pressure drop are also determined by steady-state thermal-hydraulic calculation and input to RETRAN.The algebraic slip model allowing the liquid and vapor phases to flow with unequal velocities is used to simulate the two-phase flow phenomena.

The profile fit subcooled void model is included for neutronic feedback calculation.

2-19 PXGURE 2.2.1 a 0 JET PUMP PERFORMANCE CURYE O Z 0 H l-K 0 QGI Qo 0 0 0.0 1.0 2.0 FLOH RATIO (H)

.2.3 Trip Logic The trip capability in RETRAN allows parameters (e.g., elapsed time, normalized reactor power, pressure, control block output, etc.)to be tested against a high or low threshold (trip setpoint).

The test can then be used to activate or deactivate a system.This trip logic is used in the WNP-2 RETRAN model to simulate the actuation of the Reactor Protection System (RPS)and to initiate various valves and pump actions.Table 2.3.1 provides a description of the trip logic used in the WNP-2 RETRAN model.This trip logic can be expanded to incorporate additional trips if they are needed.2-21 TABLE 2.

3.1 DESCRIPTION

OF TRIP LOGIC 01 End calculation 02'Aubine Trip (initiate stop valve closure)03 Initiate MSIV closure 05 Initiate Scram 06 Open S/R valve group 1-06 reclose S/R valve group 1 CAUSES OF TRIP ACFIVATIOÃ Simulate transient time>setpoint Control block-8 (water level)>setpoint (L8)Contml block-8 (water level)<setpoint (L2)Volte 360 (turbine inlet)pressure<setpoint Normalized power>setpoint Volume 16 (steam dc')pressure>setpoint Control block-8 (water level)<setpoint (L3)Trip 502 activated Trip 503 activate'd Volume 320 (steam line)pressure>setpoint Volte 320 (steam line)Pressure<setpoint Trips K7 thmugh+10 are used for other four S/R valve gmups 11 Trip recirculation pmps 12 Trip FW turbine 13 RCIC initiation

-13 Trip RCIC 14 Initiate HPCS-14 Trip HPCS Simulated transient time>setpoint Trip 502 activated Volwe 16 (steam deme)pressure>setpoint Control block-8 (water level)<setpoint (L2)Ccntml block-8 (water level)>setpoint (L8)Contml block-8 (water level)<setpoint (L2)Control block-8 (water level)>setpoint (L8)Contml block-8 (water level)<setpoint (L2)Contml block-8 (water level)>setpoint (L8)2-22

2.4 Control

System Models RETRAN control blocks (e.g., integrator, multiplier, function generator, etc.)provide for the simulation of a variety of reactor control systems.These control blocks can also be used to prepare combinations of parameters for editing and to perform other special functions as may be necessary.

All of the RETRAN minor edit variables are t inputs.Table 2.4.1 lists available for use as control block the control inputs used in the WNP-2 RETRAN model;The WNP-2 specific control system models are described below.2.4.1 Feedwater Control System The Feedwater Control System comprises a level control system and a feedwater flow delivery system.The level control system allows for either one-element or three-element control.In one-element control, the controller output is only a function of the difference in setpoint and sensed level.In the three-element control which is normally used, an additional steam-feed mismatch is added to the level error.All controller settings and gains are based on actual plant settings and the vendor's Control System Design Report.The feedwater delivery system is represented by the simulation of the pump flow actuator based on vendor provided plant specific information.

2-23 Figure 2.4.1 illustrates the WNP-2 Feedwater Control System model.Upon reactor scram, the Feedwater Control System switches to one-element control and the water level setpoint is lowered 18 inches.2.4.2 Pressure Control System The Pressure Control System is composed of a reactor pressure regulation system, a turbine control valve system, and a steam bypass valve system.The signals from the pressure regulation system to turbine control valve and steam bypass system can be regulated either by the difference in turbine inlet pressure and its setpoint or by the load-speed error signal.The primary settings which affect the pressure regulation system output are the regulation gain and lag-lead time constants.

They are based on vendor provided data<.The turbine-generator is not modeled and the turbine speed is specified as a function of time.Figure 2.4.2 illustrates the WNP-2 Pressure Control System model.Upon a turbine trip, the turbine control valve demand signal is grounded, thus the turbine bypass valve demand is set ecpxal to the pressure regulator demand.This will cause the bypass valves to open immediately, rather than waiting through the pressure regulator lag time constant.2-24

2.4.3 Recirculation

Flow Control System WNP-2 is operated with the recirculation flow control system set in manual control mode.No control element is required and the flow control valve position is modeled with a function generator.

2.4.4 Direct

Bypass Heating The nonconducting heat exchanger model is used to account for direct bypass heating.The heat removal rate for this heat exchanger is determined by a control system.It is assumed to be a constant fraction of the transient core power as shown in Figure 2.4.3.2-25 TABLE 2.4.1 CONTROL INPUT DEFINITION ID VARIABLE NO.SYMBOL DES CRIPFION 01 WP'*02 WP*03 LIQV 04 LIQV 05 LIQV 06 KNS 07 CONS 08 POWR 09 PRES 10 TRIP 11 KNS 12 WP"*13 PRES 18 TIMX 19 PRES 21 WQCR Steam (Jct.330)flow (8 NBR)FW (Jct.490)flow (4 NBR)Middle downccmer (Vol.18)liquid volwe (f t**3)lower downcarer (Vol.19)liquid volme (ft**3)Upper downccmer (Vol.20)liquid volume (ft*"3)Fraction of total core power deposited directly in core bypass region Constant of 1.0 active core (less core bypass)power (MW)Turbine inlet (Vol: 390)pressure (psia)Scram (trip ID=5)activation indicator Constant of 0.0 Steam (Jct.16)flow (8 NBR)Turbine stop valve inlet (Vol.360)pressure (psia)Simlation tiae (sec)Turbine bypass inlet (Vol.350)pressure (psia)Heat transferred frcm clad to coolant for core section 1 (Btu/ibm)ID No.22 through 32 are used for heat to coolant for other core sections 50 CCNS 51 TRIP 52 63NS 53 KNS Constant of 1.0 Turbine trip (ID=2)activation indicator Turbine speed ref erence (100t)load bias (10t)2-26 FXGURE 2.4.1 Feedwater Control System jIADC Va.SUM-014~LDC Vol.Llqdd Vol.(fl"3)SUM-015 FNG-118 Toblo 25 Leva!vs, Volvma SUM-086 LAG-008 Vol.12 12 Dryor Flow lFracllon ol Ralod)MUL-087 G"8.8 Sloam Dryar Prassuro Drop Corroclion hAUL 0)9 L l F{One Elemonl Conlr oil 10 Scram Acllvallon lndlcalor FXGURE 2.4.1 (CONT.)Feedwater Control System Sloam I Flow (Fraclion of Rolodl LAG-OI I G" 100.g-1.0 SUM-007 SUM"009 Filler LLG-OI0 g-l.O FW Flow (Frocllon of Rated)LAG-006 G" 100.g" 1.0 LAG-008 MUL"0l 8 Level Feedback (Three Elemenl Conlral)50 Cons."1.0 g-l.O SUM"016 g-l.O Scrom Acllvollon hdhcalor IO FIGURE 2.4.1 (CONT.)Feedwoter Control System 50 Cans.-1.0 Lovol Sol Palnl vs.Time FNG-080 Toblo I I G"563.55 Lovol Sol Down IB'flor Scram SUM-082 MUL-08 I G"-I B.IO Scram Acllvollon lndicolor g-1.0 Pl Conlr oiler SUM-004 g"-1.0 SUM-OOI G"0.0161 INT-002 G" 0.024 g-1.0 SUM"003 To FW Pump Flow Acluolor MUL-0l 9 g>>I.B FXGURE 2.4.1 (CONT.)Feedwater Control System FW Pump Flow Actuator SUM-003 SUM-120 INT-121 g-l.O SUM-122 g-l.O g-I.I5 g"-l.O g"-l.2 G" I.25 FNG"126 Toblo l4 FW Flux vs.Acluolor Oulpul G-I.25 FIGURE 2.4.2 Pressure Control System 18 Time Load vs.Time FNG-012 SUM-454 Load Bios Cons.-O.I g" 1.0 52 Turbine Speed Reference g" l.O SUM-453 g" 20.SUM"I IO Speed/Load Domond ILD)g"-l.O 18 Time FNG"452 Turbine Speed vs.Time FIGURE 2.4.2 (CONT-)Time Turbhe htel Pressure'-l.O Pressure Control System Pressure Regulator FNG-013 Pressure Selpoint vs Time g--(Pr es.Re (.-30.)SUM"04)G-O.03333 LLG-046 g-l.O LAG-040 DER-049 G-0.274 g" I.O Presswe Repvter Demand (PRO)SUM"053 p-I.O LAG-052 G-2.924 INT-05 I SUM-050 g--l.O Steom Line Compensator FXGURE.2 (CONT.)PRD 9 Pressure Control System Byposs Valve l9 Inle I Pr essur e 50 Cons." l.O 9-1.0 SUM-054 9-I.O 3%8los FNG-047 Table l9 G-4.0 LAG-055 Valve Area vs.Poslllon FNG-033 Tablo 26 MUL-032 G"-992.7 4 Prossuro Corroclion SUM"450 MUL-451 MIN-027 PRD 8ypass Valve Fill Flux LD Turbine Conlrol Volve Fil Flui 5l g"-I.O Turbine Trip Ac live lion hdlco lor LAG-029 LAG-030 VLM-025 Volvo Aroa vs.Poslllon FNG-035 Toble 27 MUL-034 G--3970.97 Pressure Carr ac lion Conlrol Valve 9 Irdul Prossure FIGURE 2.4.3 Direct Bypass Heating Acllve Core 8 Powor Cons." I.O g-l.O g--1.0 SUM"4IO I DIV-402 LAG-403 Sensed Coro Power Cons."0.02 Cons;0.02 MUL"404 G"-1.0 ldeol Aemovol Aolo for Heol Exchongor 2.5 Steady-state Initialization The RETRAN steady-state initialization option is used to initialize the model.The parameters specified for the initialization of WNP-2 model are dome pressure, core inlet enthalpy, core flows (flow through core active region and flow from lower plenum to core inlet region), recirculation flow, jet pump suction flow, feedwater and steam flows.In addition to the inputs for the thermal-hydraulic initialization, the values of the various controller setpoints and the initial output of control elements are specified.

A null transient run is performed to confirm the consistency of the thermal-hydraulic and control system initialization and to verify that the steady-state is well established.

2.6 RETRAN

Kinetics The RETRAN-,02 MOD04 code has both point kinetics and one-I dimensional kinetics capabilities.

Selection of point or one-dimensional kinetics for a given transient depends on the accuracy requirements of the simulation.

Point kinetics is used in a simulation when the axial power shape is relatively constant during the period of interest.Pressurization transients are typically analyzed with one-dimensional kinetics because the reactivity effects of void collapse and control rod movement play 2-35 an important role in determining the overall results of the calculation.

The one-dimensional kinetics model provides a more accurate calculation of these effects (particularly control rod reactivity) than the point kinetics model.The RETRAN model described herein uses nuclear cross-section information prepared by the core analysis methodology described in Reference 2.Files containing kinetics data for the various fuel types present in the reactor core are produced by CASMO-2 and three-dimensional nodal characteristics of the core are determined by SIMULATE-E

.SIMTRAN-E collapses corewide cross-sections from three-dimensional form to one-dimensional or point kinetics form as required by RETRAN.Since SIMULATE-E and RETRAN calculate moderator density differently, the SIMTRAN-E cross-sections are adjusted manually to account for thy difference.

This process is described more fully in Section 2.6.1 below.2.6.1 General Description of the Generation of One-dimensional Data The first step in the process uses the EPRI codes SIMULATE-E and SIMTRAN-E.

SIMULATE-E predicts core power and burnup distributions during detailed depletion analyses of the reactor core.Qualification of the Supply System's SIMULATE-E methodology is provided elsewhere 2-36 SIMTRAN-E was developed under EPRI sponsorship for linking SIMULATE-E and RETRAN.SIMTRAN-E reads restart files written by SIMULATE-E, extracts the appropriate information for determining cvf's the kinetics parameters, and generates the direct, RETRAN input for transient analysis.In this first step, SIMTRAN-E produces a one-dimensional kinetics data file in the form of polynomials which describe the effects of relative changes in water density and fuel temperature on calculated two-group cross sections, diffusion coefficients, inverse neutron velocities, radial bucklings, and delayed neutron fractions.

This data file could be used directly by RETRAN.However, without the adjustments described below, this approach would lead to very conservative RETRAN predictions for severe pressurization events.For benchmark analysis of pressurization events, this conservatism would create artificially large uncertainty factors.The kinetics conservatism is due to differences between the SIMULATE-E model of core average thermal hydraulics and the RETRAN model of average channel thermal hydraulics.

As a result of these difference, SIMULATE-E and RETRAN predict different changes in average moderator density for the same change in core pressure.Since SIMTRAN-E receives data only from SIMULATE-E, it cannot adjust for the differences.

Therefore, a manual adjustment is made to the SIMTRAN-E output in the second step in 2-37 the kinetics process.This step produces a revised data file consisting of a set of adjusted polynomials that can be used directly by RETRAN in the best estimate mode.Except as noted in the text, all of the transient benchmark and example analyses described in this report used the adjusted kinetics parameters as produced by the second step of the kinetics process.For transients which do, not involve a substantial change in moderator density, the adjustment is unnecessary because the induced conservatism is small.Verification of the Supply System's methodology utilizing a pre-released version of SIMTRAN-E is discussed in Section 2.6.4, below.2.6.2.Calculation of the Initial Kinetics Input Data To begin the first step in the generation of the one-dimensional data, a nominal SIMULATE-E case is run at a core configuration consistent with the initial conditions for the given transient.

This nominal SIMULATE-E case uses power and void feedback to determine the three-dimensional core power and flux distributions and the critical eigenvalue.

The nominal SIMULATE-E case uses cross-sections which have not been adjusted to match k-infinities of the lattice physics code (i.e.unadjusted Zal), but it is run from a SIMULATE-E restart file generated with cross-sections 2-38 which were adjusted to match k-infinities of the lattice physics code (i.e.adjusted Zal).For transients in which it is necessary to model the effects of control rod insertion resulting from a scram, an additional SIMULATE-E case is required.This case is based on the nominal case and is run with power feedback disabled.The only difference between this case and the nominal case is the control rod position array, which has all rods fully inserted.As noted above, SIMTRAN-E reads the restart files generated by the SIMULATE-E cases.It then collapses the three-dimensional SIMULATE-E data to one-dimensional data for RETRAN and determines the dependence of the kinetics parameters on relative water density, square root of fuel temperature, and control state.SIMTRAN-E generates all kinetics parameters except kZf>and kZf2 by radial collapse with adjoint flux weighting.

kEf]and k~f2 are radially collapsed with volume weighting.

The dependence of the kinetics parameters on water density and fuel temperature is determined by making perturbations in these quantities.

All relative water density and square root of average fuel temperature perturbations are done in three dimensions and are then radially collapsed.

The one-dimensional nominal and perturbed kinetics variables are then analyzed to produce polynomials that are functions of the relative change in water 2-39 I density and the change in the square root of the average fuel temperature at each axial node.This procedure is performed for both the nominal case and for the controlled case.2.6.3.Adjustment of Kinetics Data To begin the second step in the generation of the, one-dimensional data, the SIMTRAN-E output from the first step is used and parallel SIMULATE-E and RETRAN cases are run to quantify the difference in axial moderator density distributions between the two models for identical variations in core pressure.The coefficients in the kinetics parameter polynomials that are associated with the changes in relative moderator density are then modified so the change in each kinetics variable in RETRAN for a given pressure change js the same as that pressure change would give in the one-dimensional SIMTRAN-E model.Thus reactivity changes at each axial node generated by a pressure change are preserved between SIMTRAN-E and RETRAN.The constant term in each kinetics parameter polynomial determines the initial steady state eigenvalue in the RETRAN unperturbed state.The constant terms are not modified when new polynomial fits are developed; consequently, the SIMULATE-E eigenvalue is preserved in the RETRAN unperturbed state.2-40 The cross section libraries used in the core physics analysis are based on ENDF/B-III.

ENDF/B-III includes delayed neutron frac-tions which are artificially low.Preliminary ENDF/B-V data shows an increase in delayed neutron fraction ranging upwards from 5.44 in all fissile isotopes.To bring the delayed neutron fraction closer to those specified in ENDF/B-V, a+54 manual adjustment is applied to all delayed neutron fractions before final data is put into the RETRAN input file.2.6.4.Verification of the Supply System's Methodology The Supply System's version of SIMTRAN-E is not a formally released EPRI code.Results obtained by this version were reviewed by EI International and were found to be acceptable Further verification'as obtained by the Supply System for the steady state results by comparing the axial power distributions produced by SIMTRAN-E for the initial states of the three Peach Bottom turbine trip tests.Figures 2.6.1, 2.6.2 and 2.6.3 show the axial power shapes predicted by RETRAN compared to those predicted by SIMULATE-E and by the process computer for the initial state of each of these turbine trips.In each case, the RETRAN model is based on the one-dimensional kinetics input produced by SIMTRAN-E and modified as described above.The ultimate validation of the SIMTRAN-E calculation is the accuracy with which RETRAN predicts system behavior in benchmark 2-41 transient analyses.The transient mode is validated by the predictions of the Peach Bottom turbine trip tests, which also match the data closely.These results are shown in Section 3.2.2-42 aauaZZe.1 initial Axial Power Distribatlon Peach Bottom Unit 2 TT1 1.500 1.400 1.300 1.200 1.100 w I.OOO>0.900 Q, P&OO~0.700~g 0.600 0.500 0.400 0.300 0.200 0.100~~~~%1'I~~r~~~'.~'.~i C.r~~O'[}I(I*~~~'I'I 1 I~%1 I"-'Cr:'~~I~~~~~~',t~.~~I~1~'I~~~~~I'~r rl M Y~~~~'~~~~~I~~~'I I~%1'I1~-~~~~~~~~~I'~.~~~i I~~~~~%%r h I.':t.r: h.hr I'1~~~-~~'~~~~1~~~Ir~~\~~'I'I'r 11~"".'I I~~~~~~~~~~~~'It Ir IJ~~%'%~I 1~-'%~'1 I'I~t 1~~'I I~'I~~V I~~\I'.~:."~}.".~~~%~1~~~~~~~~~~II r Ir~I~A~I I I~~,I~~~~~~\~~.~I~r~I I i~j" cg.', I~~1~~~)~-~h~~~%'r J~~~~.~~-'}t~I~'~witt~~~t~~~~}~~~"~'I I~r~~~,I~~,\~'t%1~:..1 r}~~~~h~~It~,~~~~~}r~~'I~~~'~~~~~r}~~~~I%~~.~~~~~'.}~~~~.~~~~~hh~~~~~~~l.~~'"." I.".'I'~~~~~~~~~~>~I~I t~'~~r'.r'~rr Process RETRAN 8NULATE-E Computer-Ej-';.I.i~'.1'I 1%"~1 Ah'I~~"}'~'r'*~~'~'I~~~I I~I Irtr~~I~~h~~rh h\~~~~~~~~'~'~~~I%%%Ih ,'~~1 t'I'%~h~'I~~h~~~~r r~.~~~ih h~:::t.r~,,~~'.OOQ r~0 12 24 36 4&60 72 84 96 I 0&120 132 144 Distance Above Boffom of Active Fael (Inches)

HGURE2.5'.2 Initial Axial Power Disfrihutlon Peach Bottom Unit 2 TT2 1.500 1.400 1.300 1.200 1.100 1.000~0.900 4-0.800~0.700~g)0.600 0.500 0.400 0.300 0.200 0.100 0.000 l h I~~~~~~r~~~~~~~~~~~~~~~~~k~~'~~~~~'Lr~~~~~~h'I-r'I I~'I It tk I!~~~~~.'~l~"~~",~~~~~~~~~~~~~~<~~~: j k.r.'~~~~~~~~(~~~J~~h~I~~~~'I~~I-9~I~I~<<"" I""~I~('.~I~I'I~~~~I~~'~1'j~I'I..'rg;r~'j'~~~."" l-'.-.h ll'L~~~~~~.I~'r)~~., I~~~'I~I~I~~~h~~t't 11~h.r.rl,;"-Q~~~~r.rhr t~~~~~~I~~j I~~~tt~~~>jjk~*t..~r'/~I~~~'"""I~L~~'~~~~'I~jl~I~" 1~~~L~~~-~rI'/~~~~I~~'~~r~~~~'I'1~1 I~~~+~~~,~~l.~k~~~~t Process Computer I,"~~~~\th t tlat tent 1'I~~I I~'I j~~~~~~~~I'I~+hh ,~I't Ih'I I'I"'1 1 1~~,Ir~r~~I~;" l.'~~'I~~~I~'~L~~I~-I t I~jl Ikt~I lj~~I"I~~"L).L~.~~I'1'I\I~t~I Al lkkk ,'I A~~~~~~L~t" rt h ,~~~~~~','L~j,"~I~I~~lh I n~'~~~~~~'I 1~~~L~~~~~*AD~~~~~~~~RETRAN'IMULATE-E 1~~~~1 kr~~~II'I 1~~'I I L~'1 j~'~~~\~~~I'I 1'I 1~~rr~~~~~~'r;~~'LE~~~r I~'~~~~~L~~~'I~~~,~r~~~L~~1~*I t~~~'~L LL'~~~kl I ty~tk~~~~~I-Ml I'~~~~~~k 1 litt W I t~1\.I~'L'0 12 24 36 48 60 72 84 96 108 120 132 144 Distance Above Boffom of Active Fuel (fnches)

I=IGURE2.6.8 Initial Axial Power Distribution Peach Bottom Unit 2 TT8 1.500 1AOO 1.300 1.200 1.100<1.000~0.900<0.800~~0.700~g 0.600 0.500 OAOO 0.300 0.200 0.100 0.000~,J.I 4 J L'~~,~I~~I I'k~LJ~.~~I.l I I I ELI~J EJ~~~I'f(I~ira~~~k EIJ~I J I'k.~~J~I ,"1 I J L'~I~I I.'I J ift I~rl~~~~I~~~~I~I~~~~~~I I',~',~vhr~~~~,~~~I.~~~Ill~J~I~I ,~~~~L'.I~~~~ILE~'ll LL I.~~J~J 1~LL~I L ,~'I~~\.~~Ll~Jll~I~r~f I lt fft~I rt I I I'rt I~krt~t Ehl LI k I~LI.L~I~f I'l'~~~r~,k~'~J~~~Process Computer Jhhl 11 ,~~ggt..1~~=J I~~I~I 4~~I,'I~~l.l II I 4~~~~~I I~t ttt~, I El.lkll J I~~J~~~~I,~I~~~tr~~~I LLI~I~L El 4 I~I~~tkkl Il ik-~rrrt~I~IE4LL~1~LL I t~t Itltt, LL LJE~~~1~ttt'I I tl It I\~L 4~~I t t rt~k I'J~~EE~I I I r tt tt~I~IILIII~~I~~r I~,~'~~~I~I RETRAN SIMULATE-E

.~'I tl I~ILI~4 I~~LI I'I~E.LIEIJ II4 v'Lt'k~r I'~~~Ik~I I I I~I~~J~I~I~I,~I.I~~k~Ilk~I~ft tq f f.~~r~~E~~h~kkkkt I~I~~I'~I~LEE I~.~I~I I~J E~~.~~f r)~IJEI ELLE~1 L IL EIII fr~klh EJI~I~~I~~I~I.~I 0 12 24 36 48 60 72 84 96 108 120 132 144 Distance Above Bottom of Active Fuel (Inches)

-l l I

3.0 QUALIFICATION

The objective of this chapter is to compare the Supply System's RETRAN simulation with WNP-2 power ascension tests (PAT)and Peach Bottom turbine trip tests.The Supply System performed these benchmark analyses to qualify the WNP-2 RETRAN model and to demonstrate user qualifications.

The benchmarks comprise four WNP-2 PAT tests and three Peach Bottom turbine trip tests.These benchmark analyses, which were performed in the best-estimate mode, qualify the WNP-2 RETRAN model for the licensing basis analysis presented in the next chapter.3.1 WNP-2 Power Ascension Tests During the period of October-December 1984, a series of power ascension tests (PAT)at near full power were performed at WNP-2~~.The data from these tests is available for verifying the WNP-2 RETRAN model.All of the transients analyzed in this chapter were recorded during the initial WNP-2 PAT testing.The best-estimate model described in Chapter 2 was used in the PAT analyses and the best-estimate analyses, discussed below, verify the modeling.For future reload analysis, the licensing basis model will be used to assure conservatism in the output.The licensing basis model is discussed in Chapter 4.3-1 The power ascension tests chosen for benchmark are as follows: 1.Water level setpoint change-This transient is used mainly to benchmark the feedwater control system, water level prediction and general stability of the RETRAN model.2.Pressure regulator setpoint changes-This transient is used to benchmark the pressure regulator control system, RETRAN stability and system model accuracy.3~(One recirculation pump trip-This transient is to benchmark the pump coastdown characteristics and system response to an asymmetric recirculation flow variation.

4.Generator load rejection with bypass-This transient is used to benchmark the steam line modeling and system pressurization behavior.Since the PAT transients are milder than the limiting transients in licensing basis analysis, the first three transients were analyzed using the point-kinetics core modeling.The one-dimensional kinetics model was also run for the recirculation pump trip case to demonstrate the validity of the point kinetics model for these relatively mild events.The load rejection with bypass transient was analyzed using the 3-2 one-dimensional kinetics model.This treatment is consistent with II the example licensing basis transient analysis (load rejection without bypass)in the next chapter.3-3

3.1.1 Water

level Setpoint'hange (Test PAT 23A)The purpose of Test PAT 23A was to demonstrate the stability of the level control system.Test PAT 23A was initiated at 95.14 power and 96.84 flow.The test procedure consisted of a six-inch step increase in vessel water level setpoint, a delay to allow the system to reach a new equilibrium condition, and a six-inch step decrease in vessel water level setpoint.3.1.1.1 RETRAN Model for Test PAT 23A Since the test condition is near the rated condition, the standard RETRAN base model at rated condition as presented in Chapter 2 is used to start the transient simulation.

To model the step change of the level setpoint, a general function table used in the level setpoint control block (Control Block 80)is modified.3.1.1.2 Results and Discussions The water level setpoint step change test was analyzed mainly to qualify the feedwater control system and vessel water level models.It also confirms the adequacy of the RETRAN thermal-hydraulic and neutronic coupling.The vessel water level in this test is maintained at a specified setpoint through the variation of the feedwater flow which is 3-4

\controlled by the feedwater control system.The feedwater controller uses vessel water level and the mismatch between steam flow and feedwater flow to determine the feedwater pump speed, which controls feedwater flow.The controller responds to an increase in vessel water level setpoint by increasing feedwater'low.This increased feedwater flow causes water level in downcomer to increase and the water temperature in core inlet to decrease.The reduced core inlet temperature leads to a reduced core void, resulting in a core power increase.The feedwater controller, after detecting water level increase, will reduce feedwater flow, which leads to a reduction in power.This combination of feedwater control logic and core response will lead to a new steady state for both core power and feedwater flow close to their initial values and the water level will be stabilized at the new setpoint.Figure 3.1.1 shows the measured and calculated feedwater flow response.Similarly, Figure 3.1.2 shows the measured and calculat-ed water level.These plots show that the RETRAN model predicts events and timing consistent with the data.Figure 3.1.2 indicates that RETRAN calculates a water level that approaches a value that is six inches higher than the initial water level at about 20 seconds after the setpoint change.The measured data indicates a higher asymptotic value of 7.8 inches in water level change, which may indicate an inconsistency between the level step change used in the analysis and actual test.3-5 Other parameters (steam flow, dome pressure and core power)are not, plotted because they did not show any significant changes (less than 34 variation from steady state values)throughout the test.3-6 Figure 3.1.1 FEEDNATER FLON-PAT TEST 023 RETRAN PLANT DA A 16 SECONDS 24 32 Figure 3.1.2 HATER LEVEL-PAT TEST 023 RETRAN PLANT DA N W Zo Uf Z H 0 8 p i6 SECONOS 24 4p

3.1.2 Pressure

Regulator Setpoint Change (Test PAT 22)Test, PAT 22 was performed to demonstrate the stability of the pressure control system.Test PAT 22 was initiated at 97.54 power and 95.94 flow.The test procedure consisted of a 10-psi step decrease in pressure regulator setpoint, a delay to allow the system to reach a new equilibrium condition, and a 10-psi step increase in pressure regulator setpoint to the original value.3.1.2.1 RETRAN Model for Test PAT 22 Test PAT 22 was analyzed with the standard RETRAN base model (cf.Chapter 2).The initial dome pressure in the RETRAN base model is 1020 psia, which differs slightly from the 990-psia test pressure.The transient is very mild and the response to the step change in pressure setpoint was not expected to be sensitive to the small difference in initial pressure.To model the test, a general function table used for the pressure setpoint control block (Control Block 13)is changed to reflect the step change of the pressure setpoint.3.1.2.2 Results and Discussions Zn this test, the pressure regulator and the Digital Electro-Hydraulic Control System (DEH)will respond to a decrease in 3-9 pressure regulator setpoint by opening the turbine control valves to allow more steam flow which reduces system pressure.The resulting decreased system pressure increases core voiding and thus reduces core power.As pressure decreases, the pressure regulator and DEH control system starts to close the turbine control valve.The pressure will eventually be stablized at the new setpoint.Figure 3.1.3 shows the measured and calculated transient pressure response.The pressure settles out at about 10 psi below the initial pressure, indicating good alignment of the pressure system control model.Figure 3.1.4 presents the measured and calculated power behavior.The system stabilizes back to the initial power rapidly, and the RETRAN model predicts this behavior consistently with the data.Figure 3.1.5 shows the measured and calculated steam flow.Figure 3.1.6 presents the measured and calculated feedwater flow.The calculation matches the plant data closely in both of these areas.The simulation/data comparisons indicate that the pressure regulation control system in the WNP-2 RETRAN model performs as intended.3-10 Figure 3.1.3 OOME PRESSURE-PAT TEST 022+DOHE PRESSURE X PLAN'ATA H 0j lL OJ 8 Z r 0 x x xx x x x xxxxxxxx x 0 I p i2 TAHE (SEC)

Figure 3.1.4 NORMALIZED POWER-PAT TEST 022+BETRAN X PLANT DATA 0 lU N H J Qo K 0 Z X X XXXX x x x x x X 8 0 p i2 TrvE (sEc)

Figure 3.1.5 STEAM FLOW-PAT TEST 022+FLPM JUN 39P X PLANT DATA 0 J h.Q N~H>>J X K 0 Z X X X X Ol 0 p 12 TINE (SEC)24 Figure 3.1.6 FEEDWATER FLOW-PAT TEST 022+RETRAN X PLANT OATA 0 J U.0 N~H J X K 0 2 X X 8 0 p f2 TIME (SEC) 3.1.3 One Recirculation Pump Trip (Test PAT 30A)Test PAT 30A was performed to verify the performance of the recirculation system.The test also demonstrated that the water level could be controlled without resulting in turbine trip and/or scram.Test PAT 30A was initiated at 96.2%power and 1004 flow.The test was initiated by tripping one recirculation pump.3.1.3.1 RETRAN Model for Test PAT 30A Test PAT 30A was analyzed with the standard RETRAN base model at rated power and flow.The transient was initiated by introducing a recirculation pump trip in Recirculation Loop A at time zero.A Test PAT 30A case with one-dimensional kinetics was run to evaluate the effect of void feedback on the core power calculation at lower core flow conditions such as in this test and the results compared to the point-kinetics model.Unadjusted cross sections for Beginning of Cycle 1 conditions were used in the one-dimension-al core analysis.(See Section 2.6 for a description of cross section adjustments.)

Use of the unadj'usted cross sections is acceptable because the one-pump trip transient is very mild.The data comparison in the next section supports this assumption.

3-15 3.1.3.2 Results and Discussions The benchmark verifies the coastdown characteristics of the tripped recirculation pump and the system model response to asymmetric recirculation flow disturbances.

Neutronics, core hydraulics, pressure regulator control system, and feedwater models were validated in the analysis.Figure 3.1.7 shows measured and calculated recirculation drive flow for the tripped loop (Loop A)for the point kinetics case.Figure 3.1.8 shows measured and calculated recirculation drive flow for the unaffected loop (Loop B).The calculated flow tracks measured data in both comparisons.

The Loop B flow increases slightly as the transient is initiated and stabilizes at a higher value.The unaffected loop sees a lower flow resistance after one pump is tripped.-Figures 3.1.9 and 3.1.10 show the same comparisons for the case using one-dimensional kinetics.These comparisons are very similar to the cases with point-kinetics model, supporting the use of the point kinetics model in the other PAT test benchmarks.

Figure 3.1.11 shows the normalized jet pump flow for Loop A.Figure 3.1.12 shows the jet pump flow for Loop B.Again the RETRAN results track the data.Figures 3.1.13 and 3.1.14 are the same comparisons for the case using one-dimensional kinetics.A comparison of the one-dimensional case with the point-kinetics model showed no difference in the calculated jet pump flows.3-16 Figure 3.1.15 shows that the RETRAN core hydraulic and neutronic models calculate transient core power consistently with the data.Initial core power decrease is caused by the increased core void after the single pump trip.As the core power decreases, the core void will eventually decrease (after a fuel heat transfer time constant).

The core power begins to increase and level off at a new equilibrium.

Figure 3.1.16 is the corresponding plot for the one-dimensional RETRAN model.The one-dimensional model gives a slightly better match with the plant data than the point kinetics model later in the transient because the one-dimensional model tracks the void feedback in the core more accurately than the point kinetics model.The fluctuations observed at about 4 seconds and.16 seconds in the one-dimensional case are also the results of detailed axial void feedback.Figures 3.1.17 and 3.1.18 show the core heat flux behavior calculated by the point-kinetics model and the one-dimensional model respectively.

Both track the plant data with the one-dimensional model yielding slightly better results.3-17 Figure 3.1.7 RECIRC FLON PUNP A-PAT TEST 030A PHP A FL PLANT DA 0 J b.0 hJ N H J<e>o K 0 z 0 0 p 12 TIME, SEC 24 3p Figure 3.1.8 RECIRC FLOW PUMP B-PAT TEST 030A PHP B FL X PLANT DA A n Ul N H J<I Z~K 0 Z X X X X X X X X X X X X X X 0 0 0 12 TIME, SEC i8 24 Figure 3.1.9 RECIRC FLON PUMP 4-P4T TEST 0304-iD PNP A R.PLANT OA 0 tU N H J<e K 0 Z 0 0 0 i2 TINE, SEC 18 24 30 Figure 3.1.10 RECIRC FLON PUMP B-PAT TEST 030A-lD PHP8FL N PLANT OA A 0 hl N H J<fm>o K 0 Z X X X X X X X X X X X O 0 12 TINE, SEC is 24 30 Figure 3.l.ll JET PUMP A FLOW-PAT TEST.030A FLN JUN 1 PLANT DATA 0 Id N H J<o>o K 0 Z X X X X X X 0 I p 12 TINE, SEC Figure 3.1.12 JET PUMP 8 FLOW-PAT TEST 030A+FLON~Q x PLAtP 0ATA 3 0 h.0 llfg N~H X K 0 z x x xxxx x x x x x A OO TIHE.SEC Figure 3.1.13 JET PUMP A FLOW-PAT TEST 030A-iD FLOM 8JN i~DATA 0 bl N H J

o K 0 Z x x x X X 0 I p TIME, SEC Figure 3.1.14 JET PUMP B FLOW-PAT TEST 030A-iD+FLQI AH I x PLAUDIT olTA 0>a N~J X K O z x x xxxx xxxxx xxxxx x x a~o TIHE, SEC Figure 3.1.15 POWER-PAT TEST 030A RHRAN PLANT DA A a UJ N H J Qo K 0 Z x x x X X N 0 0 f2 vrvE, sEc 18 24 30 Figure 3.1.16 POWER-PAT TEST 030A-iD RETRAN RETRAN i PLANT DA A 0 rl II]0 Q.0 III N H J yO Qo K 0 2 x X X X X Ol 0 p TIME, SEC i8 24 30 Figure 3.l.17 CORE HEAT FLUX-PAT TEST 030A RETRAN PLANT DATA X 3 J 0.>o K 0 Z a 0 p TINE, SEC 24 Figure 3.1.18 CORE HEAT FLUX-PAT TEST 030A-io BETRAN 1 PLANT DA A 0 rl X 3 J tL~p>o K 0 z p 0 p 6 12 TINE, SEC 3p

3.1.4 Generator

Load Rejection With Bypass (Test PAT 27)Test PAT 27 was initiated at 97.54 power and 95.44 flow.The transient was started by the activation of the main generator trip pushbutton.

The rapid closure of the turbine control valves pressurizes the steam lines and the core.As the void collapses, positive void reactivity is induced.Scram is initiated by the turbine control valve fast closure pressure switch.The early scram results in negative overall reactivity throughout the test.The net effect is a power decrease shortly after the initiation of the transient.

The turbine control valve closure also initiates the recirculation pump trip (RPT).The turbine control valve closure and subsequent steamline pressurization activate the opening of the turbine bypass valves to relieve vessel pressure.Since the capacity of the bypass is less than the test power level, dome pressure continues to increase.Eventually the SRVs open to limit the pressure rise.For this event Group 1 SRVs opened.3.1.4.1 RETRAN Model for Test PAT 27 The main generator trip is set at 0.0 seconds.The turbine control valve performance was taken from the test data.In the WNP-2 3-30 RETRAN model a single valve (Junction 380)at the end of steam line simulates both turbine control and stop valves.When the control valve fast closure is activated, its corresponding delay time and closure time are input so that Junction 380 simulates a control valve..Observed control rod performance data was used as the RETRAN scram time.The maximum bypass flow for the base deck is set at the design value of 254 of rated steam flow.Plant data supports a value of I 37%maximum bypass flow, which was used for this simulation.

I The one-dimensional kinetics model was used in this simulation.

As mentioned in Section 3.1.3, for a mild transient as in this case, uncorrected one-dimensional cross sections are sufficient.

3.1.4.2 Results and Discussions Figure 3.1.19 shows the calculated and measured variation in the Average Power Range Monitor (APRM)signal during Test PAT 27.The APRM signal is proportional to the neutron flux.The output from RETRAN is adjusted so that the decay power is subtracted from the total power before it is compared to the measured data.Test PAT 27 is the only benchmarked power ascension test which resulted in a reactor scram.Figure 3.1.19 shows that the RETRAN prediction tracks the initiation and progress of the scram closely, 3-31

~~indicating acceptable scram modeling.The WNP-2 RETRAN model contains two separate recirculation loops.Figure 3.1.20 and 3.1.21 show that RETRAN follows the rates of decrease for both loops.The lower flow predicted for Loop B is due to uncertainty of delay time for RPT initiation and a RETRAN deficiency which results in calculating slightly asymmetrical loop flows in a symmetric system with symmetric transient conditions.

However, the differences in flows are small.They are not expected to affect the overall accuracy of the simulation.

Figure 3.1.22.compares the calculated and measured core flow.The results verify the capability to calculate recirculation loop and core flows after a Recirculation Pump Trip (RPT).Figure 3.1.23 shows measured and calculated dome pressure during the test.Turbine control and stop valve closure causes a rapid system pressurization.

RETRAN predicts the pressure transient accurately, particularly during the early stages of the transient (0-4 seconds)when the fuel thermal behavior is important for the thermal limit predictions.

The measured pressure spike at 0.3 seconds appeared only in the wide range Division 2 signal;wide range Division 1 and narrow range signals do not show this deviation.

The apparent pressure spike may have been an instrument aberration.

The plant data shows that one relief valve opened while a second one opened and closed repeatedly.

The WNP-2 RETRAN model treats the first two SRVs with lowest pressure setpoint as a 3-32 single equivalent valve.Both SRVs opened in the RETRAN simulation and the RETRAN pressure results are lower after about 5 seconds.Figure 3.1.24 shows the steam flow variation.

The oscillation in the flow rate from 0 to 3 seconds is caused by pressurization waves after the turbine control and stop valves are closed.3-33 Figure 3.1.19 POHER-PAT TEST 027+POXGl IO NINCTIC X PLANT CATA K lU 0 Q 0 llI N M J XK o Oo 2 0 0 0 4 TIME, SEC Figure 3.1.20 RRC FLON A-PAT TEST 027+PLlW All ROT-SD)(PLANT DATA X X X 0 0 3 0 h.0 UJ N M X K 0 Z 4 0 0 D 4 TINE.SEC Figure 3.1.21 RRC FLOH B-PAT TEST 027+PLON~404-lO X PlANT OATA 0 h.0 ill N H J X K 0 Z r 4 X X X X X X X X X X 0 0 O 4 TIME, SEC Figure 3.1.22 TOTAL CORE FLOW-PAT TEST 027 0 0 U.0 hl N M J E K 0 z'O x x x 0 O y 4 TIHE, SEC Figure 3.1.23 OOME PRESSURE-PAT TEST 027+PAICS 10 KINETIC X PLANl'ATA IU K Ul ll)Ill o ga Lo xxxxx x x x x x x x x x x x x 0 0 4X 4 TIHE, SEC Figure 3.1.24 STEAM FLOW-PAT TEST 027+aa iso n.ox sn X PLAHz 0ATA 3 0 h.0 Ill N H J X K 0 z O X X x x X x x X x X x X X X O O y 4 TIME, SEC

3.2 Peach

Bottom Turbine Trip Tests Benchmarking of the WNP-2 RETRAN model to the power ascension test measurements verifies the capability and accuracy of most elements in the model.These benchmarks cover expected operation, but normal startup testing does not cover circumstances which challenge the core operating limits.To demonstrate the overall capability of the RETRAN model under design basis conditions, the Supply System performed an analysis of the three pressurization transient tests.(TT1,-TT2, TT3),conducted at Peach Bottom Atomic Power Station Unit 2 (PB2).3.2.1 Test Description Detailed accounts of the Peach Bottom turbine trip tests can be found in the EPRI report.A brief description is given here.Turbine trip tests TT1, TT2 and TT3 were performed at PB2 prior to shutdown for refueling at the end of cycle 2 in April 1977.These tests were conducted jointly by Philadelphia Electric Company, GE and EPRI to investigate the effect of the pressure transient generated in the reactor vessel following a turbine trip on the neutron flux in the reactor core.Measurements of major process variables such as core pressure, dome pressure and neutron flux were recorded at a frequency of 166 samples a.3-40 second.These measurements provide the best set of data for the qualification of transient analysis methods.The tests were initiated by manually tripping the turbine (turbine stop valve closure)at three reactor power levels and near rated core flow.The turbine stop valve (TSV)position scram signal was intentionally delayed to allow a significant neutron flux transient to take place in the core, providing adequate qualification data.The power increase was terminated by a trip of the reactor protection system on high neutron flux.To maintain sufficient operating margin, the APRM high neutron flux scram setpoint was set down closer to the initial reactor power level.The initial reactor power, core flow and the APRM scram setpoint for each test are shown in Table 3.2.1.TABLE 3.2.1 PEACH BOTTOM TURBINE TRIP TESTS TEST CONDITIONS POWER CORE FLOW APRM SETPOINT TEST~MW Rated Mlbm hr Rated 0 Rated TT2 TT3 1562 2030 2275 47.4 61.6 69.1 101.3 82.9 101.9 98.8 80.9 99.4 85 95 77 3-41

3.2.2 Peach

Bottom Unit 2 Model Description The Peach Bottom model incorporates the modeling techniques of the WNP-2 model.A schematic of the model is shown in Figure 3.2.(The WNP-2 model is shown in Figures 2.1 through 2.4.)The nodalization within the reactor vessel is identical except that the two downcomer volumes are combined into one in the Peach Bottom model.Also the two recirculation loops are combined into one in the Peach Bottom model and the recirculation loop is represented by two nodes whereas the WNP-2 model has five nodes for each recirculation loop.The Peach Bottom model includes the entire main steam bypass system whereas the WNP-2 model uses a negative fill junction.This model is the best estimate bypass system model of Hornyik and Naser , and was included to provide a realistic simulation of this component.

Because the steam line geometry has a significant effect on pressurization transients, the geometric data for the steam line from Philadelphia Electric Company's topical report was used.The Peach Bottom steam line is modeled with six nodes whereas the WNP-2 steam line is modeled with seven nodes.An additional node was used in the WNP-2 model to provide more accurate pressure for SRVs lifting.SRVs did not open during the Peach Bottom turbine trip tests.The physical dimensions and-characteristics of the dominant fuel type were used.The dimensions and characteristics for the dominant 7x7 fuel type were obtained from EPRl documentation 3-42 PXGURE 3.2 PB2 RETRAN MODEL 10 19 Feed-waler 2 Loops 13 p;26, 25 j~5l 30 34 12 14 SRVs 15 Slop valves C onlrol valves 27'8 i 29 18 Recirculalion pumps I MSIVs 17 Bypass valves 31 9 Lines 20 Condenser 32 33

3.2.3 Initial

Conditions and Model Inputs Since comparison with actual measurements was a primary objective, best estimate model inputs developed from original data sources such as drawings and measured plant performance data were used.The core thermal power, total core flow, core inlet enthalpy and initial steam flow were obtained from the process computer P-1 edits taken before each transient test.The steam dome pressures were obtained from the recorded data.The recirculation system was adjusted to correspond to the initial reactor conditions.

The core bypass flow was calculated for each test with the SIMULATE-E MOD03 (" SIMULATE-E")

computer code.The loss coefficient at the core bypass region entrance was also adjusted to match the core plate pressure drop calculated by SIMULATE-E.

Reactor water levels were initialized to match the test data.Table 3.2.2 lists the initial conditions for each test of the Peach Bottom analyses.The feedwater flow rate was specified as a constant value for each test.The short duration of the tests minimizes the potential effects of the feedwater control system.The constant flow assumption was validated through an additional analysis using feedwater flow characteristics provided by Philadelphia 3-44 Electric Company.Both analyses provided the same results for transient power and pressure responses.

The control rod scram time and speed can be estimated from the measured plant Rod Position Information System drift relay output signals.The average of the measured scram speeds (a sample of 31 of the 185 control rods from TT1)is plotted in Re'ference 18 and was used with correction for rod acceleration for all three tests.All of the control rods were assumed to insert at the average speed.The measured time dependent Turbine Stop Valve (TSV)position and the Turbine Bypass Valve (BPV)position were used as RETRAN input.A linear TSV opening was assumed with the stroke time obtained from measured data.The BPV flow area was assumed to be proportional to the measured position.Since the TSV position signal channel malfunctioned during TTl, the average of the signals from TT2 and TT3 was used.Since the Peach Bottom Turbine trip tests were pressurization transients, they were analyzed using the one-dimensional kinetics model.The SIMULATE-E code was used to generate the RETRAN one dimensional kinetics data at the initial conditions for each test.A stepwise depletion of cycles 1 and 2 based on the EPRI documentation was used to determine the fuel exposure, void history and control history at the time of the tests.The basic 3-45 procedures described in Section 2.6 were used to develop each of the three sets of kinetic data.TABLE 3.2.2 PEACH BOTTOM TURBINE TRIP TESTS INITIAL CONDITIONS TT2 TT3 Core Thermal Power (MW)1562'2030.0 275.0 Total Core Flow (ibm/sec)Core Bypass Flow (ibm/sec)Core Plate Pressure Drop (psid)Steam Dome Pressure (psia)Core Inlet Enthalpy (Btu/ibm)Steam Flow (ibm/sec)Recirculation Flow (ibm/sec)16'991.6 528.0 1628.0 ll.61 976.1 518.1 17.71 986'521.6 2183'2461'9386.0 7686.0 9443.0 28139.0 23028.0 28306.0 1636'0 1384.87 1762.75 3-46

3.2.4 Comparison

with Measurements The goal of these Peach Bottom analyses was to demonstrate the Supply System's RETRAN model of PB2 can accurately simulate the power and pressure increase during rapid pressurization transient.

Therefore, comparisons of RETRAN calculations to the measured pressures (turbine inlet, steam dome and upper plenum)and LPRM signals are essential.

They are presented in the following two sections.3.2.4.1 Pressure Comparisons Pressure comparisons are expressed in terms of pressure change from the initial value.This eliminates the need to account for the sensing line elevation head, uncertainties in the pressure loss coefficient and differences between nodal and local pressures.

Pressure transients calculated at three locations are compared with the measured values in Figures 3.2.1 through 3.2.3 (at the turbine inlet), Figures 3.2.4 through 3.2.6 (at steam dome), and Figures 3.2.7 through 3.2.9 (at core upper plenum).The measured pressures are obtained directly from the test data file and have not been.filtered.Time shifts (to account for sensing line delay)based on information provided in the EPRI documentation were applied to the calculated pressures.

To eliminate the 3-47 instrument line effects, the RETRAN model calculated upper plenum pressures are compared to the filtered test data in Figures 3.2.10 through 3.2.12.The good agreements.in turbine inlet pressures and steam dome pressures indicate that the dynamic of the steam lines is well simulated.

The first pressure oscillation in the steam dome is slightly overpredicted for TT1 and slightly.underpredicted for TT2 and TT3.The upper plenum pressure calculated by RETRAN for TT1 is slightly higher than.the measured data.For TT2 and TT3, the calculated and measured upper plenum pressures agree'reasonably well.Adequate prediction of the core upper plenum pressure response is essential to transient power predictions.

Table 3.2.3 summarizes the calculated and measured steam dome and upper plenum pressures at the peak of first oscillation.

Overall, the RETRAN calculated pressures are in good agreement with the measured data.The discrepancies are within the tolerances due to uncertainties in RETRAN model inputs such as initial steam flow, bypass valve opening delay and turbine stop valve closing time.3-48 TABLE 3.2.3 PEACH BOTTOM TURBINE TRIP TESTS PRESSURE CHANGE (PSI)AT PEAK OF FIRST OSCILLATION CALC.DATA STEAM DOME UPPER PLENUM CALC.DATA 34.7 40.5 46.2 33.4 41.9 47.4 37.5 42.3 48.3 34.9 44.2 49.9 3-49 FIGURE 3.2.1 PB TTi TURBINE INLET PRESSURE HEASURED RETRAN ld 8 2+O QItI N W K 0.O I 0 I p Tlute (sec)

FIGURE 3.2.2 PB TT2 TURBINE INLET PRESSURE H Ro g 8 ld 8 z io On(N W K Q.o Ol I o o I p TIME (SEC j FIGURE 3.2.3 PB TT3 TURBINE INLET PRESSURE HEASURED RETRAN IIJ 8 Z*a Qa N hl K IL O N I O I p TINE (SEC)

FIGURE 3-2.4 PB TT1 STEAM DOME PRESSURE HEASURED RETRN O IQ H N tL hJ 8 Z~z 0 N lU K fL 0 0.TIME (SEC)

FIGURE 3.2 5 PB TT2 STEAN DONE PRESSURE}KASUREO H N Q.O td 8 Z x D O~'f N Ol K Q.O 0 TIME (SEC}

FIGURE 3.2.6 PB TT3 STEAN DOME PRESSURE HEASURED H N IL 0 Id 8 Z z 0 O~'f U)Id K Q.O ill O 0 TINE (SEC)

PXGURE 3.2.7 PB TTi UPPER PLENUM PRESSURE MEASURED BETA AN 0 6 H N Q.M 8 ZQ<<f'f x 0 N hJ K Q.0 0 Tree (sec)

FIGURE 3.2.8 O O PB TT2 UPPER PLENUM PRESSURE H 8 0.0 ld 8 z Z 0 O~V S lU K Il O g O 0 nuc (sec)

FIGURE 3.2.9 O 0 PB TT3 UPPER PLENUM PRESSURE H N Q O hl 8 2 x 0 O~'i S W K Q.0 0 TINE f SEC)

FIGURE 3.2.10 PB TTI UPPER PLENUM PRESSURE MEAS.(FILTERED)

RETRAN N IvPu K Q.O 0.0 0.6 TINE (SEC)1.2 FIGURE 3.2 11 0 l0 PB TT2 UPPER PLENUM PRESSURE HEAS.tf ILTEREO)RETRAH H Ujo N UJPu K IL D.D 0.6 Tzvc (sec)

FIGURE 3.2.12 O a PB TT3 UPPER PLENUN PRESSURE HEAS.(f ILTERED)RETRAH 0.0 0.6 Tree (sec) 3.2.4.2 Power an/Reactivity Comparisons The calculated core average neutron powers are compared to the normalized core average LPRM signals for each of the three tests in Figures 3.2.13 through 3.2.15.In all three cases, the rates of power change, timing trends and power peak magnitudes are in good agreement with the measured data.The capability to predict the power transients was further evaluated by comparing the area under the power peak during the pressurization transients to that predicted by RETRAN.In the thermal margin calculation, the critical power ratio is a function of.the area under the power peak, not the magnitude of the peak.Tables 3.2.4 presents a summary of the calculated and measured power peaks and the area under the peaks for each test.A comparison of the time of the calculated and measured power peaks is given in Table 3.2.5.The LPRM detectors are located at four elevations (from bottom to top, levels A, B, C, D).Comparisons of calculated flux to measured flux (average of all LPRMs at a level)at each axial level are presented in Figures 3.2.16 through 3.2.27.The calculated and measured peak values at each level is summarized in Table 3.2.6.Timing trend and relative peak magnitude are predicted well in the individual LPRM levels.This demonstrates that RETRAN is capable of predicting accurately the power shape change during rapid pressurization transient.

3-62 The calculated net.reactivity, scram reactivity, and net reactivity implied by the data are presented in Figures 3.2.28 through 3.2.30.The implied net reactivity was calculated using an inverse point kinetic algorithm and the average of the measured LPRM signals.Table 3.2.7 summarizes the calculated and implied peak reactivities.

The agreement between the calculated and the implied net reactivities is good.The slight overprediction of the peak reactivity for all three tests is caused by the overprediction of the upper plenum pressure at the time of peak reactivity.

It is noted that the magnitudes of the overpredictions in reactivity are small relative to those of the neutron power.This is due to the extreme sensitivity of the neutron power to.changes in reactivity close to the prompt critical condition.

The reactivity figures also show that the calculated TT1 and TT2 net reactivity turns before scram occurs while TT3 net reactivity is turned by scram.The same trends are observed for the implied net reactivities.

3-63 TABLE 3.2.4 PEACH BOTTOM TURBINE TRIP TESTS

SUMMARY

OF CORE AVERAGE PEAK NEUTRON'POWER PEAK NEUTRON POWER (NORM)CALC.DATA O'IFF.AREA UNDER PEAK CALC.DATA DIFF.5.41'.68 5.39 4.83 4.54 4.90 12.0 3.1 10.0 0.960 0.769 0'17 0.743 3.5 0.669 7.2 0.888 8.1 TABLE 3.2.5 PEACH BOTTOM TURBINE TRIP TESTS TIME (SEC)OF PEAK NEUTRON POWER CALC.DATA TT1 TT2 TT3.774.720.702.774.726.702 3-64 TABLE 3.2'PEACH BOTTOM TURBINE TRIP TESTS

SUMMARY

OF LPRM LEVEL NEUTRON POWER PEAKS CORE D AVG.Calculation Data 4 Diff.3'2 3.48 6.90 4.98 4.46 11.'7 5.99 5.23 14.5 6.15 5.59 10.0 5.41 4.83 12.0 Calculation Data 4 Diff.3.49 3.52-0.9~4.68 4.50 4.0 5.09 4'1 3~7 4.82 5.02-.4.0 4.68 4.54 3.1 Calculation Data 4 Diff.3.84 3.68 4.3 5.42 4.83 12.2 6.06 5.45 11.2 5.74 5.47 4.9 5.39 4.90 10.0 3-65 TABLE 3.2.7 PEACH BOTTOM TURBINE TRIP TESTS REACTIVITY

SUMMARY

PEAK REACTIVITY

($)TIME OF PEAK (SEC)CALC.DATA DIFF.CALC.DATA 0.804 0.780 0.836 0;776 0.767 0.812 3.6%1.74 2.54 0.738 0.690 0.678 0.744 0.696 0.660 3-66 FIGURE 3.2.13 PB TTI CORE AVERAGE POWER K W 0 ll 0 bJ N H Z K 0 z 0 0.0 0.6 lIME (SEC)

FIGURE 3.2.14 PB TT2 CORE AVERAGE PONER HEASUREO RETAAN 0 MN H J X K 0 z 0.0 0.6 TIME (SEC)1.2 FIGURE 3.2.15 PS TT3 CORE AVERAGE PONER HEASURED RETRAN K IU 0 Q.0 hl N H J X K 0 Z 0.0 0.6 nate (sec)i.2 FIGURE 3.2.16 PB TTi LEVEL A AVERAGE LPRM HEASURED RHHAN 0 hl N H J X K 0 Z 0.0 0.6 TDIE (SEC)

FIGURE 3.2.17 PB TTI LEVEL B AVERAGE LPRM 0 IdH J Z K 0 Z 0.0 0.6 TIME (SEC)

FIGURE 3.2.18 PB TTi LEVEL C AVERAGE LPRM K LU 0 Q.0 hl N H J X K 0 z 0.0 0.6 TINE (SEC)

FIGURE 3.2.19 PS TTi LEYEI 0 AYERAGE ARM 0 W N Z K 0 z 0.0 0.6 TIME (SEC)

FIGURE 3.2.20 PB TT2 LEVEL A AVERAGE LPRM 8SUAED p AHRN 0 ld J Z K 0 z 0.0 0.6 nHE (sEc)i.2 FIGURE 3.2.21 PB TT2 LEVEI B AVERAGE ARM REASUREDC RETRAN K IIJ 0 Q.0 td N H J Z K 0 z 0.0 0.6 TINE (SEC)1.2 FIGURE 3.2.22 PB TT2 LEVEL C AVERAGE LPRM 0 tUN J X K 0 Z 0.0 0.6 TIME (SEC)

FIGURE 3.2.23 PB TT2 LEVEL D AVERAGE LPRM 0 hl N J X K 0 z 0 0.0 D.6 , TIME (SEC)

FIGURE 3.2.24 PB TT3 LEVEL A AVERAGE LPRM n td H J X K 0 Z 0.0 0.6 TINE (SEC)

FXGURE 3.2.25 PB TT3 LEVEL B AVERAGE LPRM n td N H X K 0 Z 0.0 0.6 TIHE (SEC)

FIGURE 3.2.26 PB TT3'LEVEL C AVERAGE LPRM 0 lU J X K 0 Z 0.0 0.6 TINE (SEC)

FIGURE 3.2.27 PB TT3 LEVEL D AVERAGE ARM HEASURED RETAN K IU g 0 0 lUN J X K 0 z 0.0 0.6 TINE (SEC)1.2 FIGURE 3.2.28 O PB TTl REACTIVITY HEASUAED RET.TOTlL 6RA Cl 0 I-HQ)o H 0 IU K tll O I N 0 I 0.0 0,6 TIME (SEC)f.2 FIGURE 3.2.29 PB TT2 REACTIVITY HEASURED RET.TOTaL ERAH l0 0 HN>o H I" 0 UJ K Ol O I 8 O I 0.0 0.6 TIME (SEC)

FIGURE 3.2.30 0 PB TT3 REACTIYITY HEASURED BET.TOTAL a 0 0-I-Hol>o I" 0 IIJ K Ol 0 I 0 O 0.0 0.6 Trwe (sec)

4.0 LICENSING

BASIS ANALYSIS A broad spectrum of transient events have been analyzed for WNP-2;the results are presented in the Final Safety Analysis Report.These events cover a wide range of scenarios and conditions contributing to Technical Specification Limits.Most of these transient events are not sensitive to changes in reload core configuration, or are within the conservative limits established by the original FSAR analy'sis.

Changes in fuel design and core configuration are usually bounded by the analysis of selected limiting events.Based on previous analyses performed by vendors for WNP-2+and utilities on similar plants , the two most limiting events requiring a reanalysis with each reload core are: 1.Load Rejection Without Bypass (LRNB)2.Feedwater Controller Failure to Maximum Demand (FWCF)The results of these transients generally determine Technical Specification limits for minimum critical power ratio (MCPR).This chapter describes the system analysis for these transients.

The full licensing FSAR analysis, the sensitivity analysis and the hot channel analysis from which the operating limits are obtained will be described in a separate applications topical report (to be submitted later).The purpose of including this section is merely to indicate the parameters that typically change in modelling conservative FSAR transients and to show the WNP-2 model, with the parameters modified, indeed calculates conservative results.4-1

4.1 Licensing

Basis Model The licensing basis model described in this chapter is a generic model using the Cycle 4 core configuratiop.

For future applica-tions, specific reload configurations and plant parameters will be used.These calculations are typical of planned WNP-2 reload analyses.The licensing basis RETRAN model is'a modification of the WNP-2 best-estimate model.The modifications assure the cons'ervatism of the calculated results by using the values of the key parameters which bound the expected operating range.Table 4.1 compares licensing basis model.inputs with the nominal values.The nominal values and conditions show conservatism in the licensing basis modeling.The licensing analysis performed in this report uses the end-of-cy-cle exposure for the calculation of the nuclear design data.At EOC, control rods are withdrawn from the core to counteract the consumption of excess reactivity.

The average control rod scram distanc'e is greater with more rods withdrawn, so scram performance degrades near the end of cycle.Scram reactivity insertion rate is the dominant power reversal phenomenon for pressurization tran-sients;the most severe results occur at the maximum cycle exposure, when scram performance is least effective.

4-2 l 1 TABLE 4.1 INPUT PARAMETERS AND INITIAL TRANSIENT CONDITIONS COMPARISON OF LICENSING BASIS AND NOMINAL PLANT CONDITIONS Parameter Nominal Licensin Basis Core Exposure Thermal Power (MWt)Steam Flow (lbs/sec)BOC-EOC 3323 3970.97 Feedwater Flow Rate (lbs/sec)3970.97 EOC 3468 4161.11 4161.11 Feedwater Temperature

('F)Vessel Dome Pressure (psia)Rod Insertion Speed Core Inlet Enthalpy (Btu/lb)Fuel Rod Gap Conductance 420'020 Measured 527.6 Axially Non-uniform 424 1035 Tech.Spec.529.3 Uniform Jet Pump Ratio 2.33 Safety/Relief Valves Relief Function (psig)Fuel Radial Heat Generation Non-uniform Uniform 2.41 Group 1 Group 1 Group 2 Group 2 Group 3.Group 3 Group 4 Group 4 Group 5 Group 5 Opening Closing Opening Opening Setpoint Closing Setpoint Opening Setpoint Closing Setpoint Opening Setpoint Closing Setpoint Opening Setpoint Closing Setpoint Opening Setpoint Closing Setpoint, Stroke Time (sec)Stroke Time (sec)Delay Time (sec)1076 1026 1086 1036 1096 1046 1106 1056 1116 1066 0.07 0.0 0.3 1106 1056 1116 1066 1126 1076 1136 1086 1146 1096 0.1 0.0 0.4 a.RETRAN will adjust this value at initialization to complete the heat balance.4-3 TABLE 4.1 INPUT PAEVLHETERS AND INITIAL TRANSIENT CONDITIONS COMPARISON OF LICENSING BASIS AND NOMINA)PLANT CONDITIONS (Continued)

Parameter Nominal Licensin Basis Safety/Relief Valves Safety Function (psig)Group 1 Group 1 Group 2 Group 2 Group 3 Group 3 Group 4 Group 4 Group 5 Group 5 Opening Closing Opening Opening Setpoint Closing Setpoint Opening Setpoint Closing Setpoint Opening Setpoint Closing Setpoint Opening Setpoint Closing Setpoint Opening Setpoint Closing Setpoint Stroke Time (sec)Stroke Time (sec)Delay Time (sec)1150 1126 1175 1151~.1185 1161 1195 1171 1205 1181 0.07 0.0 0.3 1177 1153 1187 1163 1197 1173 1207 1183 1217 1193 0.1 0.0 0.4 Reactor Protection System High Flux Scram, 4 NBR 118 High Vessel Dome Pressure 1037 Scram (psig)APRM Thermal Trip (4 NBR 113.5 at 1004 Core Flow)Low, Water Level (L3), in 13 above instrument zero Turbine Stop Valve Closure 5 Position Scram (4 Closed)MSIV Closure Position Scram 10 (4 Closed)126 2 1071 122.03 7.5 10 15 4 4 TABLE 4.1 INPUT PAEQMETERS AND INITIAL TRANSIENT CONDITIONS COMPARISON OF LICENSING BASIS AND NOMINAL PLANT CONDITIONS (Continued)

Parameter Containment Isolation and Pump Trip Low Water Level (L2), in below instrument zero Low Pressure in Steamline (psig)RPT High Vessel Pressure (psig)RPT Delay Time (msec)High Water Level-Turbine and Feedwaters Pump Trip (inches above instrument zero)Recirculation Pump Moment of Inertia (10~ibm-ft~)Nominal 50 831" 1135 97 54.5 2.27 Licensin Basis 70 795 1170 190 59.5 2.47 I 4-5 The analyses.in this report used the technical specification limits on control rod movement versus time.Table 4.2 shows the assumed rod motion following scram+.Actual plant performance data shows more rapid insertion.

TABLE 4.2 Technical Specification Limits Maximum Control Rod Insertion Time to Position After Deenergization of Pilot Valve Solenoids Position Inserted from Full Withdra Notch Number Time~Sec 6.254'8'754'7.924'9.584'45)

(39)(25)(05)0.430 0.868 1.936 3.497 The initial steam flow in the licensing basis model is conserva-tively set at 1054 NBR.For pressurization transients, higher initial steam flow results in a more rapid pressurization and higher maximum pressures.

The initial power is set to 104.44 NBR which is consistent with the maximum steam flow of 1054 NBR.The initial reactor dome pressure is conservatively set to a higher value of 1035 psia, allowing less analytical margin to the safety limit.Unless the problem statepoint requires otherwise, the core flow is initialized at the rated capacity of 108.5 mlb/hr.4-6 The RETRAN model uses a fuel rod gap conductance that remains constant during the transient.

The actual gap conductance increases during power increase transients due to fuel pellet expansion.

Higher gap conductance will lead to faster heat transfer from the fuel to the coolant, which generates more steam voids.The faster conversion of fuel stored energy to steam voids in the core helps to mitigate the transient due to negative void reactivity feedback.Therefore, the use of a constant gap conductance is conservative for system analyses involving power increases such as pressuriza-tion transients.

Conservative equipment design specifications and plant technical specification limits are used in the RETRAN model input.These include relief valve opening response, closure rates for main steam isolation valves, turbine stop and control valves, reactor protection system setpoints and delays.A conservative moment of inertia for the recirculation pump is used in the licensing basis model.A larger value results in longer coastdown time after pump trip, delaying the effect of void formation in the core and increasing the process of void collaps-ing.Positive reactivity effects are magnified by this conserva-tism.l 4-7 4.2 Load Rejection Without Bypass (LRNB)Whenever external disturbances result in loss of electrical load on the generator, fast closure of the turbine control valves (TCV)is initiated.

The turbine control valves are required to close as rapidly as possible to minimize overspeed of the turbine generator rotor.Closure of the main turbine control valves will cause a sudden reduction in steam flow which results in an increase in system pressure and reactor shutdown.4.2.1 Sequence of Events A loss of generator electrical load at high power with bypass failure produces the sequence of events listed in Table 4.3.The closure characteristics of the turbine control valves are assumed such that the turbine control valves operate in the full arc (FA)mode and have a full stroke closure time, from fully open to fully closed, of 0.15 seconds.Sensitivity study" has shown that the most severe initial condition for this transient is the assumption of full arc operation at 1054 NBR steam flow.The plant value of 0.07 seconds given in Table 4.3 represents actual expected closure time, since the turbine control valves are partially open during normal operation.

4-8 TABLE 4.3 Sequence of Events for LRNB Transient Time-Sec Event 0.0 Turbine generator power load unbalance (PLU)devices trip to initiate turbine control valve fast closure when loss of electrical load is detected.0.0 Turbine bypass valves fail to operate 0.0 0.0 0.07 0'9 Fast turbine control valve closure initiates scram trip Fast turbine control valve closure ini-tiates a recirculation pump trip (RPT)Turbine control valves closed Recirculation pump motor/circuit breakers open, causing decrease in core flow 0.28 1.35 1.40 1.44 1.50 1.63 4.43 5.0 Control rod insertion starts (scram trip signal at 0 sec, RPS delay: 0.08 sec, solenoid deenergizing delay: 0.2 sec)Group 1 relief valves actuated Group 2 relief valves actuated Group 3 relief valves actuated Group 4 relief valves actuated Group 5 relief valves actuated Group 5 relief valves close End of simulation 4-9

4.2.2 Results

of LRNB RETRAN Analysis The WNP-2 LRNB analysis at the end of cycle 4 conditions was performed with the licensing basis model.Since most.of the fuel in the core at EOC4 was the Advanced Nuclear Fuels (ANF)design, the average fuel parameters in the best-estimate model were changed from the GE design to the ANF design.The fast closure of the turbine control valves (TCV)is simulated by linearly decreasing the flow at fill Junction 380 (representing steam flow to the turbine)to zero at 0.07 seconds.Rapid closure of the TCV initiates a scram.Several key results of this analysis were compared with analyses of record performed by Advanced Nuclear Fuels (ANF).Zt should be noted that both sets of analyses were performed conservatively.

This comparison is intended to show the similarity of results rather than to demonstrate analytical accuracy.The accuracy of the WNP-2 RETRAN model is demonstrated by the benchmarks of power ascension tests reported in Section 3.1.The pressure in the steam line increases rapidly as shown in Figure 4.2.1.The acronym"LRNB LBM" in the figure stands for Load Rejection without Bypass Licensing Basis Model.Figure 4.2.2 shows the vessel steam flow.The flow oscillations are caused by the pressure wave propagated upstream to the reactor vessel.The decreased steam flow at about 0.4 seconds causes the rapid 4-10 pressurization of the steam dome and inside the core as shown in Figures 4.2.3, 4.2.4 and 4.2.5.After 0.42 seconds, the net reactivity becomes positive because the positive void reactivity exceeds the negative scram reactivity.

Zt peaks with a value of approximately 0.76$at 0.78 seconds then begins to decrease as the scram reactivity increases, as shown in Figure 4.2.6.The ANF prediction~~

of dome pressure during the transient is also shown in Figure 4.2.3.The WNP-, 2 RETRAN model predicts a pressure which is.higher than that predicted by ANF throughout the tran-sient.The reactor power, shown in Figure 4.2.7, increases rapidly and reaches a peak value of 3984 NBR at 0.89 seconds then rapidly decreases as Doppler feedback and scram reactivity terminate the power excursion.

ANF's prediction of core power is also shown in Figure 4.2.7.The power history predicted by RETRAN peaks earlier in the transient than the ANF prediction at a lower maximum power level.The earlier power peak can be attributed in part to the higher pressure throughout the transient.

The lower magnitude of the peak is likely to be caused by differences in neutronics calculations leading to differences in kinetics data and cross sections.Figure 4.2.8 shows the core average clad surface heat flux.The initial reduction in clad-to-coolant heat transfer is caused by the 4-11 rise in saturation temperature of the liquid phase due to initial pressure rise in the core.As the power rises, the heat flux quickly reverses and begins to rise, reaching a peak of 133.44 of the rated power value at 1.1 seconds.Following the peak, the heat flux decreases as the core power decreases with a delay determined by the fuel rod time constant.ANF's calculation of core average heat flux is also shown in Figure 4.2.8.The two models predict consistent trends in heat flux and agree closely in the later part of the transient.

t The water level and feedwater flow during LRNB are shown in Figures 4.2.9 and 4.2.10.When the TCV fast closure calls for scram, the feedwater controller reduces the water level setpoint by 18 inches.It then responds to this setpoint change by reducing feedwater flow.Pressure variations, steam flow oscillations, and void collapse contribute to the changing water level throughout.

the remainder of the transient.

Figures 4.2.11 and 4.2.12 give the void fractions at mid-core and core exit.Core voids collapse as the steamline pressure wave.reaches the core.For the remainder of the transient, variations in steam flow and pressure drive oscillations in the void fraction.Figure 4.2.13 shows the recirculation flow.The recirculation pumps start to coast down after RPT initiation at 0.19 seconds, causing flow reduction in the core as shown in Figure 4.2.14.4-12 FIGURE 4.2.1 WNP-2 LRNB LBM-STEAMLINE PRESSURE T IHE (SEC)

FIGURE 4.2.2 WNP-2 LRNB LBM-VESSEL STEAM FLOW 2 TIHE (SEC)

FIGURE 4.2.3 HNP-2 LANB LBM-OOME PRESSURE+PACQI-VOL$4)(AMP CALO%ATION O a 0 llJ K D N Ul taboo[f rs Q~I y TIME (SEC)

FIGURE 4.2.4 NNP-2 LRNB LBM-PRESSURE (MID-CORE) 0 N M Ul Q UJ K U)N tuoo 0.'eo Q%I O O 0~I O 2 TIME (SEC)

FIGURE 4.2.5 WNP-2 LRNB LBM-PRESSURE (CORE EXIT)O O a~I Id K D Q Q ejo (f Pe g rl O O O~i e TIME (SEC)

FIGURE 4.2-6 NNP-2 LRNB LBM-TOTAL REACTIVITY

+TQZAL REACTIVITY I-H>>+I H l O W K TIHE (SEC)

FIGURE 4.2.7 HNP-2 LRNB LBM-CORE POHER+CORC PNKA g ANF CALCAATIOtl K lU 0 Q.o a 0 TIME (SEC)

FIGURE 4.2.8 HNP-2 LRNB LBM-CORE AVERAGE HEAT FLUX K e z R Xo Del b.O 4O TIHE (SEC)

FIGURE 4.2.9 O r WNP-2 LRNB LB M-L I Qu XO LEVEL 2 H tU gO~II 0 H 3 U M O"o TIME[SEC)

FIGURE 4.2.10 WNP-2 LRNB LBM-FEEDWATER FLOW TIME (SEC)

FIGURE 4.2.11 WNP-2 LRNB LBM-VOID FRAC (MID-COREJ

+VOIO FRAC VQ..5$z O H I-K h.0 Og Q~4O TIME (SEC)

FIGURE 4.2-12 HNP-2 LRNB LBM-VOID FRAC (CORE EXIT)O z 0 H I-O 4o gl Q.o 0 M O O Q Oo TINE (SEC)

FIGURE 4.2.13 WNP-2 LRNB LBM-RECIRCULATION FLOW X 0<o O C7 0 TIME (SEC)

FIGURE 4.2.14 WNP-2 LRNB LBN-CORE INLET FLOW O 4 0 O Ro-TIHE (SEC)

4.3 Feedwater

Controller Failure to Maximum Demand (FWCF)This analysis postulates the feedwater controller failure causing an increase in feedwater flow.The most severe event of this type is a failure at maximum flow demand.The feedwater controller is forced to its upper limit at the beginning of the event.4.3.1 Sequence of Events When feedwater flow exceeds steam flow, the water.level rises.With the feedwater controller disabled, the water level eventually rises to the high-level reference point, at which time the feedwater pumps and the main turbine are tripped and a scram is initiated.

Table 4.4 lists the sequence of events for this transient.

The transient is simulated by programming an upper limit failure in the feedwater system such that 146 percent feedwater flow occurs at the design pressure of 1020 psig.An increase in feedwater flow will cause a corresponding drop in feedwater temperature.

However, the relatively large time constant of the feedwater heaters (order of minutes)plus the flow transport time (about 10 seconds from heaters to vessel and about 3 seconds from sparger to core)delay the cold water effects until the event has run its course and no further consequences are expected.4-27 Feedwater temperature is therefore assumed to remain constant.4.3.2-Results of FWCF RETRAN Analysis The FWCF event was analyzed at EOC4 conditions using the licensing basis model.As in the LRNB case, the fuel parameters were changed to reflect the ANF design.The feedwater flow is shown in Figure 4.3.1..The increased feedwa-ter,.after a transport delay through the lower downcomer and recirculation loops, causes an increase in the core inlet subcool-ing as shown in Figure 4.3.2.The reactor water level also increases as the feedwater flow increases as shown in Figure 4.3.3.The water level reaches the high level setpoint at approximately 17.7 seconds, causing a turbine trip (Figure 4.3.4).The vessel pressure begins to increase after the closure of the turbine stop valves.The turbine bypass valves open (Figure 4.3.5).For high initial power levels the bypass, which has a design capacity of 254 of rated steam flow, will not divert all of the steam flow and the pressure increases as shown in Figure 4.3.6.As the pressure increases, the core void collapses.

The positive void reactivity from core pressurization is initially high enough to overcome the negative scram reactivity (Figure 4.3.7).A rapid increase in power begins at 18.1 seconds (Figure 4.3.8), reaching a peak of 2454 NBR at 18.6 seconds.Trailing the reactor power, the core average heat flux peaks at 1244 NBR at 18.8 seconds (Figure 4.3.9).4-28 The relief valves open after the vessel pressure reaches the opening setpoints (Figures 4.3.10 through 4.3.14)and additional steam is relieved to the suppression pool.The vessel pressure begins to decrease rapidly.Figure 4.3.15 shows the vessel steam flow.The fast closure of the turbine stop valves generate pressure waves which lead to the oscillations in steam flow.The core inlet flow and exit flow are shown in Figures 4.3.16 and 4.3.17.Due to the coastdown of the recirculation pumps, the core flow reduces near the end of the transient (Figure 4.3.18).Figures 4.3.19 and 4.3.20 show the mid-core and core exit pressures.

Figures 4.4,.21 and 4.4.22 show the mid-core and core exit void fractions.

The transient is terminated by the Doppler feedback and the control rod scram.The RETRAN results were not compared with ANF analyses of record for the FNCF transient because different initial conditions were assumed in the two analyses.The ANF analysis assumed an initial power level of 474 of rated, while the example calculation reported here was performed at an initial power level of 104.44 of rated.4-29 TABLE 4.4 Secpxence of Events for Feedwater Controller Failure Time-Sec Event Initiate simulated failure of 146%upper limit on feedwater flow 17.60 17.66 17.67 L8 vessel Level setpoint trips feedwater pumps L8 vessel level setpoint trips main turbine.Turbine bypass operation initiated Reactor scram trip actuated from main turbine stop valve position switches (104 closure)17.86 19.12 19.33 19.39 19'7 19 70 20.56 20.90 21.74 23.49 24.0 Group 2 relief valves Group 3 relief valves actuated actuated Group 4 relief valves actuated Group 5 relief valves actuated Group 5 relief valves start to close Group 4 relief valves start to close Group 3 relief valves start to close Group 2 relief valves start to close End of simulation Recirculation pump trip (RPT)actuated by stop valve position switches (104 closure)Group 1 relief valves actuated 4-30 FIGURE 4.3.1 WNP-2 FWCF LBM-FEEOWATER FLOW TINE (SEC)je FIGURE 4.3.2 HNP-2 FHCF LBM-CORE INLET SUBCOOLING S I-Q No H 0 0 O Q N TIME (SEC)f4 FIGURE 4.3.3 WNP-2 FWCF LBM-LIQUIO LEVEL mg 0 H D H TIME (SEC)f4 FIGURE 4HNP-2 FHCF LBM-TURBINE STEAM FLQN TIHE (SEC)

FIGURE 4.3.5 WNP-2 FWCF LBM-TURBINE BYPASS FLOW K S z R x O<o r TIME tSEC)

PXGURE 4.3.6 WNP-2 FWCF LBM-DOME PRESSURE lU K M Q+o 0:ro Q O O O~I y TIHf (SEC)ie FIGURE 4.3-7 WNP-2 FWCF LBM-TOTAL REACTIVITY HD>o H I-O QJ K R I O TIME (SEC)

FIGURE 4.3.8 WNP-2 FWCF LBM-CORE POWER K llJ X O Q 0 TIHE (SEC)Ce FIGURE 4.3.9 WNP-2 FWCF LBM-CORE AVERAGE'HEAT FLUX.TIME tSEC)i4 FIGURE 4.3-10 NNP-2 FHCF LBM-GROUP l.SRV FLOW.TIHE (SEC)

FIGURE 4.3.11 WNP-2 FWCF LBM-GROUP 2 SRV FLOW 3 0<o TIME (SEC)

FIGURE 4.3.12 WNP-2 FWCF LBM-GROUP 3 SRV FLOW 0 4o TIME (SEC)

FIGURE 4.3.13 WNP-2 FWCF LBM-GROUP 4 SRV FLOW TIME (SEC)

FIGURE 44 WNP-2 FWCF LBM-GROUP 5 SRV FLOW TIHE (SEC)

FIGURE 4.3.15 WNP-2 FWCF LBM-VESSEL STEAM FLOW ALON~SfO.TIHE (SEC)

FIGURE 4.3.16 WNP-2 FWCF LBM-CORE INLET FLOW TIHE (SEC)14 FIGURE 4.3.17 O~I WNP-2 FWCF LBM-CORE EXIT FLOW m z 1C'0 0 h.O 4O TI HE (SEC)$4 FIGURE 4.3.18 WNP-2 FWCF LBM-RECIRCULATION FLOW K m z TAHE (SEC)

FIGURE 4.3.19 WNP-2 FWCF LBM-PRESSURE tMED-CORE)

O O 0 tlJ K lO 0)~O QPo Q O A O'IME (SEC)

FIGURE 4.3.20 NNP-2 FHCF LBH-PRESSURE (CORE EXIT)H M Q lU K D 0)M QJ 0 gas g tl O O e~I 0 TIHE (SEC)

FIGURE 4.3.21 WNP-2 FWCF LBM-VOID FRAC (MID-CORE) z O H I O K h.0 H 0 a OO TINE (SEC)

FXGURE 4.3.22 WNP-2 FWCF LBM-VOID FRAC (CORE EXIT)Z 0 H I-O K h.0 H 0 O 0 O O TIME (SEC)

4.4 Summary

of Transient Analysis The key transient simulation.

results for the two MCPR limiting transients as calculated by RETRAN are summarized in Table 4.5.TABLE 4.5 Summary of Thermal-Limiting Transient Results LRNB FWCF Max Power (%NBR)Time at'ax power (seconds)Max core avg heat flux (4NBR)Time at max heat flux (seconds)Max dome pressure (psia)Time at max dome pressure (sec)398 0.89 133 1207 1~9 245 18.6 124 18.8 1175 19.5 4-53 I I I I I 5.0

SUMMARY

AND CONCLUSIONS Benchmark analyses covering specific Power Ascension Tests as described in Section 3.1 demonstrate the capability of the WNP-2 RETRAN model to predict core and system behavior during normal operation and mild transients.

These analyses validate the modeling of the feedwater and pressure regulator control systems and the performance of the recirculation pumps, jet pumps, and steam lines as modeled for,WNP-2.

Benchmark analyses covering the turbine trip tests performed at Peach Bottom 2 at the end of Cycle 2 as described in Section 3.2 demonstrate RETRAN's ability to model conditions more challenging than the WNP-2 startup tests and the Supply System technical staff's competence to perform these analyses.These analyses validate the capabilities of the modeling beyond the normal operating envelope of the reactor.Example calculations covering typical limiting transients as reported in Chapter 4 demonstrate the WNP-2 RETRAN model's ability to predict system performance under conditions which challenge operating limits.These analyses show consistency with existing analyses of record and validate the Supply.System technical staff's ability to formulate and analyze limiting transient events.5-1 The analyses performed in this report demonstrate the ability of the WNP-2 RETRAN model and the qualifications of the Supply System technical staff to predict the course of a wide variety of transient events.The model is applicable to the evaluation of normal-and anticipated operation for plant operational support and core reload analysis.5-2

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