Validation of the turbulence models in the DLR TAU code for transonic flows: a best practice guide
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| Main Author: | |
|---|---|
| Format: | Book |
| Language: | English |
| Published: |
Köln
DLR, Abt. Unternehmensorganisation und -information
2006
|
| Edition: | Als Ms. gedr. |
| Series: | Forschungsbericht / Deutsches Zentrum für Luft- und Raumfahrt e.V.
2006,1 |
| Subjects: | |
| Online Access: | Inhaltsverzeichnis |
| Physical Description: | IX, 105 S. graph. Darst. |
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| adam_text | FORSCHUNGSBERICHT 2006-01 VALIDATION OF THE TURBULENCE MODELS IN THE DLR
TAU CODE FOR TRANSONIC FLOWS - A BEST PRACTICE GUIDE TOBIAS KNOPP
DEUTSCHES ZENTRUM FUR LUFT- UND RAUMFAHRT INSTITUT FUR AERODYNAMIK UND
STROMUNGSTECHNIK GOTTINGEN 106SEITEN 28 BILDER 0 TABELLEN 45
LITERATURSTELLEN ULB DARMSTADT ILLLLLLLLLLLLLLLLLLLLLLL 16322032
DEUTSCHES ZENTRUM DLR FUR LUFT- UND RAUMFAHRT E.V IN DER
HELMHOLTZ-GEMEINSCHAFT CONTENTS ZUSAMMENFASSUNG VIII ABSTRACT IX 1
INTRODUCTION 1 1.1 BACKGROUND: THE DLR PROJECT HIGHPERFLEX 1 1.2 CFD
CODE-VALIDATION AND BEST-PRACTICE GUIDELINES 2 1.3 SCOPE 2 1.4 SURVEY OF
THE STATE OF KNOWLEDGE 2 1.4.1 VERIFICATION, VALIDATION AND
BEST-PRACTICE GUIDELINES 2 1.4.2 VALIDATION OF TURBULENCE MODELS FOR
TRANSONIC AERODYNAMICS ... 3 1.5 SUMMARY OF THE UNDERLYING APPROACH 4
1.6 IMPORTANCE AND NOVELTY 4 1.7 OUTLINE 4 1.8 HOW TO USE THIS REPORT 5
1.9 ACKNOWLEDGEMENTS 5 1 FUNDAMENTALS 6 2 INTRODUCTION TO THE DLR TAU
CODE 7 2.1 THE NUMERICAL METHOD 7 2.1.1 GOVERNING EQUATIONS 7 2.1.2
SEMI-DISCRETISATION IN SPACE USING FVM 8 2.1.3 DISCRETISATION IN TIME 8
2.1.4 NON-LINEAR SOLVER. RUNGE-KUTTA AND LUSGS 9 2.1.5 CONVERGENCE
ACCELERATION. MULTIGRID AND RESIDUAL SMOOTHING .. 10 2.2 STATISTICAL
TURBULENCE MODELLING IN THE DLR TAU CODE 13 2.2.1 AN OVERVIEW OF
APPROACHES FOR TURBULENCE MODELLING 13 2.2.2 IMPLEMENTED MODELS FOR THE
REYNOLDS STRESS TENSOR 14 IV 2.2.3 THE SPALART-ALLMARAS TYPE
ONE-EQUATION MODELS 15 2.2.4 THE LINEAR FC-W-TYPE TWO-EQUATION MODELS 17
2.2.5 EXPLICIT ALGEBRAIC REYNOLDS STRESS MODELS 20 3 VERIFICATION AND
VALIDATION OF CFD SIMULATIONS 25 3.1 CONCEPTS AND TERMINOLOGY 25 3.1.1
MODELLING AND SIMULATION 25 3.1.2 VERIFICATION AND VALIDATION 25 3.1.3
SOURCES OF INACCURACIES IN NUMERICAL SOLUTIONS 26 3.1.4 ERROR AND
UNCERTAINTY 27 3.1.5 AIM OF VERIFICATION AND VALIDATION 28 3.1.6 BEYOND
THE SCOPE OF V&V: PREDICTION FOR FUTURE APPLICATION ... 29 3.2 QUALITY
CRITERIA FOR A CFD SIMULATION 30 3.2.1 ACCURACY 30 3.2.2 SOME REMARKS ON
THE ACCURACY OF EXPERIMENTAL DATA 33 3.2.3 STATISTICAL APPRAISAL OF
TURBULENCE MODELS 34 3.2.4 CONVERGENCE BEHAVIOUR 36 3.3 TEST CASE
VALIDATION DATABASE 40 3.3.1 VALIDATION PHASES IN HIGHPERFLEX 40 3.3.2
BENCHMARK CASES 41 3.4 BEST PRACTICE GUIDELINES 42 3.4.1 ROLE OF
TURBULENCE MODELLING 44 3.4.2 ROLE OF THE NUMERICAL SCHEME (FLOW SOLVER)
44 II VALIDATION 46 4 NACA64A010 SHOCK STALL CAS E (SSC) 47 4.1
DESCRIPTION OF THE TEST CASE 47 4.2 CONVERGENCE AND ACCURACY FOR THE
STEADY STATE CASE 48 4.2.1 OBJECTIVES 48 4.2.2 CRITERIA FOR CONVERGENCE
48 4.2.3 QUANTIFICATION OF ACCURACY 49 4.2.4 SUMMARY OF RESULTS FOR
CONVERGENCE 49 4.2.5 SUMMARY OF RESULTS FOR ACCURACY 50 4.2.6
BEST-PRACTICE GUIDELINES FOR NACA64A010 SSC (STEADY STATE) .. 51 4.3
APPENDIX FOR THE NACA64A010 SSC STEADY STATE CASE 54 4.3.1 RESULTS FOR
CONVERGENCE BEHAVIOUR 54 4.3.2 RESULTS FOR ACCURACY 55 4.4 NACA64A010
SSC FORCED HARMONIC MOTION 57 4.4.1 DESCRIPTION OF THE TEST CASE 57
4.4.2 REVIEW OF INSTATIONARY AERODYNAMICS 58 4.4.3 OBJECTIVES 59 4.4.4
CRITERIA FOR CONVERGENCE 59 4.4.5 SUMMARY OF RESULTS FOR CONVERGENCE 60
4.4.6 SUMMARY OF RESULTS FOR ACCURACY 61 4.4.7 BEST-PRACTICE GUIDELINES
FOR NACA64A010 SSC (FORCED PITCHING) 62 4.5 APPENDIX FOR THE NACA64A010
SSC FORCED HARMONIC MOTION 64 4.5.1 RESULTS FOR NUMERICAL ERROR DUE TO
TIME DISCRETIZATION AND INNER ITERATION 64 4.5.2 RESULTS FOR ACCURACY 65
RAE2822 CASE 10 69 5.1 DESCRIPTION OF THE TEST CASE 69 5.2 CONVERGENCE
AND ACCURACY 70 5.2.1 OBJECTIVES 70 5.2.2 CRITERIA FOR CONVERGENCE 70
5.2.3 QUANTIFICATION OF ACCURACY 71 5.2.4 SUMMARY OF RESULTS FOR
CONVERGENCE 71 5.2.5 SUMMARY OF RESULTS FOR ACCURACY 72 5.2.6
BEST-PRACTICE GUIDELINES FOR RAE2822 CASE 10 73 5.3 APPENDIX:
CONVERGENCE AND ACCURACY FOR RAE2822 CASELO 76 5.3.1 RESULTS FOR
CONVERGENCE BEHAVIOUR 76 5.3.2 RESULTS FOR ACCURACY 77 NLR7301 80 6.1
NLR7301 STEADY STATE (AGARD) 80 6.1.1 DESCRIPTION OF THE TEST CASE 80
6.1.2 CONCERGENCE BEHAVIOUR 80 6.1.3 CENTRAL SOLVER VS. UPWIND SOLVER 81
6.1.4 ACCURACY 82 6.1.5 PREDICTION OF FLOW SEPARATION 83 6.2 NLR7301
STEADY STATE (MP2084) 85 6.2.1 DESCRIPTION OF THE TEST CASE 85 6.2.2
SOME REMARKS ON WIND-TUNNEL EFFECTS IN MP2084 85 6.2.3 CONCERGENCE
BEHAVIOUR 86 6.2.4 ACCURACY AND SENSITIVITY ANALYSIS 86 6.2.5 PREDICTION
OF FLOW SEPARATION 87 6.3 BEST PRACTICE GUIDELINES FOR NLR7301 88 6.4
APPENDIX FOR THE NLR 7301 90 6.4.1 NLR7301 STEADY STATE (AGARD) 90 6.4.2
SENSITIVITY ANALYSIS FOR THE NLR 7301 MP2084 91 III BEST-PRACTICE
GUIDELINES 93 7 BEST PRACTICE GUIDELINES 94 7.1 CHECK-LIST FOR ENSURING
ROBUSTNESS 94 7.2 CHECK-LIST FOR MINIMIZING NUMERICAL ERRORS 94 7.3 BEST
PRACTICE GUIDELINES FOR FLOW SOLVER (NUMERICAL PART) 97 7.4 BEST
PRACTICE GUIDELINES FOR TURBULENCE MODELS 98
|
| adam_txt |
FORSCHUNGSBERICHT 2006-01 VALIDATION OF THE TURBULENCE MODELS IN THE DLR
TAU CODE FOR TRANSONIC FLOWS - A BEST PRACTICE GUIDE TOBIAS KNOPP
DEUTSCHES ZENTRUM FUR LUFT- UND RAUMFAHRT INSTITUT FUR AERODYNAMIK UND
STROMUNGSTECHNIK GOTTINGEN 106SEITEN 28 BILDER 0 TABELLEN 45
LITERATURSTELLEN ULB DARMSTADT ILLLLLLLLLLLLLLLLLLLLLLL 16322032
DEUTSCHES ZENTRUM DLR FUR LUFT- UND RAUMFAHRT E.V IN DER
HELMHOLTZ-GEMEINSCHAFT CONTENTS ZUSAMMENFASSUNG VIII ABSTRACT IX 1
INTRODUCTION 1 1.1 BACKGROUND: THE DLR PROJECT HIGHPERFLEX 1 1.2 CFD
CODE-VALIDATION AND BEST-PRACTICE GUIDELINES 2 1.3 SCOPE 2 1.4 SURVEY OF
THE STATE OF KNOWLEDGE 2 1.4.1 VERIFICATION, VALIDATION AND
BEST-PRACTICE GUIDELINES 2 1.4.2 VALIDATION OF TURBULENCE MODELS FOR
TRANSONIC AERODYNAMICS . 3 1.5 SUMMARY OF THE UNDERLYING APPROACH 4
1.6 IMPORTANCE AND NOVELTY 4 1.7 OUTLINE 4 1.8 HOW TO USE THIS REPORT 5
1.9 ACKNOWLEDGEMENTS 5 1 FUNDAMENTALS 6 2 INTRODUCTION TO THE DLR TAU
CODE 7 2.1 THE NUMERICAL METHOD 7 2.1.1 GOVERNING EQUATIONS 7 2.1.2
SEMI-DISCRETISATION IN SPACE USING FVM 8 2.1.3 DISCRETISATION IN TIME 8
2.1.4 NON-LINEAR SOLVER. RUNGE-KUTTA AND LUSGS 9 2.1.5 CONVERGENCE
ACCELERATION. MULTIGRID AND RESIDUAL SMOOTHING . 10 2.2 STATISTICAL
TURBULENCE MODELLING IN THE DLR TAU CODE 13 2.2.1 AN OVERVIEW OF
APPROACHES FOR TURBULENCE MODELLING 13 2.2.2 IMPLEMENTED MODELS FOR THE
REYNOLDS STRESS TENSOR 14 IV 2.2.3 THE SPALART-ALLMARAS TYPE
ONE-EQUATION MODELS 15 2.2.4 THE LINEAR FC-W-TYPE TWO-EQUATION MODELS 17
2.2.5 EXPLICIT ALGEBRAIC REYNOLDS STRESS MODELS 20 3 VERIFICATION AND
VALIDATION OF CFD SIMULATIONS 25 3.1 CONCEPTS AND TERMINOLOGY 25 3.1.1
MODELLING AND SIMULATION 25 3.1.2 VERIFICATION AND VALIDATION 25 3.1.3
SOURCES OF INACCURACIES IN NUMERICAL SOLUTIONS 26 3.1.4 ERROR AND
UNCERTAINTY 27 3.1.5 AIM OF VERIFICATION AND VALIDATION 28 3.1.6 BEYOND
THE SCOPE OF V&V: PREDICTION FOR FUTURE APPLICATION . 29 3.2 QUALITY
CRITERIA FOR A CFD SIMULATION 30 3.2.1 ACCURACY 30 3.2.2 SOME REMARKS ON
THE ACCURACY OF EXPERIMENTAL DATA 33 3.2.3 STATISTICAL APPRAISAL OF
TURBULENCE MODELS 34 3.2.4 CONVERGENCE BEHAVIOUR 36 3.3 TEST CASE
VALIDATION DATABASE 40 3.3.1 VALIDATION PHASES IN HIGHPERFLEX 40 3.3.2
BENCHMARK CASES 41 3.4 BEST PRACTICE GUIDELINES 42 3.4.1 ROLE OF
TURBULENCE MODELLING 44 3.4.2 ROLE OF THE NUMERICAL SCHEME (FLOW SOLVER)
44 II VALIDATION 46 4 NACA64A010 SHOCK STALL CAS E (SSC) 47 4.1
DESCRIPTION OF THE TEST CASE 47 4.2 CONVERGENCE AND ACCURACY FOR THE
STEADY STATE CASE 48 4.2.1 OBJECTIVES 48 4.2.2 CRITERIA FOR CONVERGENCE
48 4.2.3 QUANTIFICATION OF ACCURACY 49 4.2.4 SUMMARY OF RESULTS FOR
CONVERGENCE 49 4.2.5 SUMMARY OF RESULTS FOR ACCURACY 50 4.2.6
BEST-PRACTICE GUIDELINES FOR NACA64A010 SSC (STEADY STATE) . 51 4.3
APPENDIX FOR THE NACA64A010 SSC STEADY STATE CASE 54 4.3.1 RESULTS FOR
CONVERGENCE BEHAVIOUR 54 4.3.2 RESULTS FOR ACCURACY 55 4.4 NACA64A010
SSC FORCED HARMONIC MOTION 57 4.4.1 DESCRIPTION OF THE TEST CASE 57
4.4.2 REVIEW OF INSTATIONARY AERODYNAMICS 58 4.4.3 OBJECTIVES 59 4.4.4
CRITERIA FOR CONVERGENCE 59 4.4.5 SUMMARY OF RESULTS FOR CONVERGENCE 60
4.4.6 SUMMARY OF RESULTS FOR ACCURACY 61 4.4.7 BEST-PRACTICE GUIDELINES
FOR NACA64A010 SSC (FORCED PITCHING) 62 4.5 APPENDIX FOR THE NACA64A010
SSC FORCED HARMONIC MOTION 64 4.5.1 RESULTS FOR NUMERICAL ERROR DUE TO
TIME DISCRETIZATION AND INNER ITERATION 64 4.5.2 RESULTS FOR ACCURACY 65
RAE2822 CASE 10 69 5.1 DESCRIPTION OF THE TEST CASE 69 5.2 CONVERGENCE
AND ACCURACY 70 5.2.1 OBJECTIVES 70 5.2.2 CRITERIA FOR CONVERGENCE 70
5.2.3 QUANTIFICATION OF ACCURACY 71 5.2.4 SUMMARY OF RESULTS FOR
CONVERGENCE 71 5.2.5 SUMMARY OF RESULTS FOR ACCURACY 72 5.2.6
BEST-PRACTICE GUIDELINES FOR RAE2822 CASE 10 73 5.3 APPENDIX:
CONVERGENCE AND ACCURACY FOR RAE2822 CASELO 76 5.3.1 RESULTS FOR
CONVERGENCE BEHAVIOUR 76 5.3.2 RESULTS FOR ACCURACY 77 NLR7301 80 6.1
NLR7301 STEADY STATE (AGARD) 80 6.1.1 DESCRIPTION OF THE TEST CASE 80
6.1.2 CONCERGENCE BEHAVIOUR 80 6.1.3 CENTRAL SOLVER VS. UPWIND SOLVER 81
6.1.4 ACCURACY 82 6.1.5 PREDICTION OF FLOW SEPARATION 83 6.2 NLR7301
STEADY STATE (MP2084) 85 6.2.1 DESCRIPTION OF THE TEST CASE 85 6.2.2
SOME REMARKS ON WIND-TUNNEL EFFECTS IN MP2084 85 6.2.3 CONCERGENCE
BEHAVIOUR 86 6.2.4 ACCURACY AND SENSITIVITY ANALYSIS 86 6.2.5 PREDICTION
OF FLOW SEPARATION 87 6.3 BEST PRACTICE GUIDELINES FOR NLR7301 88 6.4
APPENDIX FOR THE NLR 7301 90 6.4.1 NLR7301 STEADY STATE (AGARD) 90 6.4.2
SENSITIVITY ANALYSIS FOR THE NLR 7301 MP2084 91 III BEST-PRACTICE
GUIDELINES 93 7 BEST PRACTICE GUIDELINES 94 7.1 CHECK-LIST FOR ENSURING
ROBUSTNESS 94 7.2 CHECK-LIST FOR MINIMIZING NUMERICAL ERRORS 94 7.3 BEST
PRACTICE GUIDELINES FOR FLOW SOLVER (NUMERICAL PART) 97 7.4 BEST
PRACTICE GUIDELINES FOR TURBULENCE MODELS 98 |
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| id | DE-604.BV021562986 |
| illustrated | Illustrated |
| index_date | 2024-07-02T14:35:23Z |
| indexdate | 2024-07-09T20:38:42Z |
| institution | BVB |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-014778903 |
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| physical | IX, 105 S. graph. Darst. |
| publishDate | 2006 |
| publishDateSearch | 2006 |
| publishDateSort | 2006 |
| publisher | DLR, Abt. Unternehmensorganisation und -information |
| record_format | marc |
| series2 | Forschungsbericht / Deutsches Zentrum für Luft- und Raumfahrt e.V. |
| spelling | Knopp, Tobias 1975- Verfasser (DE-588)128593938 aut Validation of the turbulence models in the DLR TAU code for transonic flows a best practice guide Tobias Knopp DLR-FB-2006,1 Als Ms. gedr. Köln DLR, Abt. Unternehmensorganisation und -information 2006 IX, 105 S. graph. Darst. txt rdacontent n rdamedia nc rdacarrier Forschungsbericht / Deutsches Zentrum für Luft- und Raumfahrt e.V. 2006,1 Turbulente Strömung (DE-588)4117265-6 gnd rswk-swf Numerische Strömungssimulation (DE-588)4690080-9 gnd rswk-swf Transsonische Strömung (DE-588)4135633-0 gnd rswk-swf Transsonische Strömung (DE-588)4135633-0 s Turbulente Strömung (DE-588)4117265-6 s Numerische Strömungssimulation (DE-588)4690080-9 s DE-604 Deutsches Zentrum für Luft- und Raumfahrt e.V. Forschungsbericht 2006,1 (DE-604)BV011758990 2006,1 HEBIS Datenaustausch Darmstadt application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=014778903&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
| spellingShingle | Knopp, Tobias 1975- Validation of the turbulence models in the DLR TAU code for transonic flows a best practice guide Turbulente Strömung (DE-588)4117265-6 gnd Numerische Strömungssimulation (DE-588)4690080-9 gnd Transsonische Strömung (DE-588)4135633-0 gnd |
| subject_GND | (DE-588)4117265-6 (DE-588)4690080-9 (DE-588)4135633-0 |
| title | Validation of the turbulence models in the DLR TAU code for transonic flows a best practice guide |
| title_alt | DLR-FB-2006,1 |
| title_auth | Validation of the turbulence models in the DLR TAU code for transonic flows a best practice guide |
| title_exact_search | Validation of the turbulence models in the DLR TAU code for transonic flows a best practice guide |
| title_exact_search_txtP | Validation of the turbulence models in the DLR TAU code for transonic flows a best practice guide |
| title_full | Validation of the turbulence models in the DLR TAU code for transonic flows a best practice guide Tobias Knopp |
| title_fullStr | Validation of the turbulence models in the DLR TAU code for transonic flows a best practice guide Tobias Knopp |
| title_full_unstemmed | Validation of the turbulence models in the DLR TAU code for transonic flows a best practice guide Tobias Knopp |
| title_short | Validation of the turbulence models in the DLR TAU code for transonic flows |
| title_sort | validation of the turbulence models in the dlr tau code for transonic flows a best practice guide |
| title_sub | a best practice guide |
| topic | Turbulente Strömung (DE-588)4117265-6 gnd Numerische Strömungssimulation (DE-588)4690080-9 gnd Transsonische Strömung (DE-588)4135633-0 gnd |
| topic_facet | Turbulente Strömung Numerische Strömungssimulation Transsonische Strömung |
| url | http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=014778903&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
| volume_link | (DE-604)BV011758990 |
| work_keys_str_mv | AT knopptobias validationoftheturbulencemodelsinthedlrtaucodefortransonicflowsabestpracticeguide AT knopptobias dlrfb20061 |