Holdings: Explanation of AEROSTABIL limit-cycle oscillations via high-fidelity aeroelastic simulations

Explanation of AEROSTABIL limit-cycle oscillations via high-fidelity aeroelastic simulations:

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Bibliographic Details
Main Author:	Stickan, Bernd (Author)
Format:	Thesis Book
Language:	English
Published:	Köln DLR, Deutsches Zentrum für Luft- und Raumfahrt 2018
Edition:	Als Manuskript gedruckt
Series:	DLR, Deutsches Zentrum für Luft- und Raumfahrt Forschungsbericht 2018-23
Subjects:	Transsonische Strömung Schwingung Flattern > Technik Computersimulation Aerodynamik Grenzzykel Numerische Strömungssimulation Fluid-Struktur-Wechselwirkung Aeroelastizität Hochschulschrift
Online Access:	Inhaltsverzeichnis Inhaltsverzeichnis
Physical Description:	188 Seiten Illustrationen, Diagramme 21 cm

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adam_text	CONTENTS 1. INTRODUCTION 27 1.1. STATE OF THE A R T............................................................ 30 1.2. OBJECTIVES..................................................................... 32 1.3. THESIS OUTLINE ............................................................ 33 2. CONCEPTS AND PRINCIPLES 35 2.1. STATIC A EROELASTICITY................................................... 36 2.2. DYNAMIC AEROELASTICITY ............................................. 36 2.3. LIMIT-CYCLE-OSCILLATIONS............................................. 38 2.3.1. DAMPER NONLINEARITY....................................... 39 2.3.2. AERODYNAMIC AMPLITUDE DEPENDENCY .... 39 3. METHODS AND TOOLS 41 3.1. COMPUTATIONAL FLUID DYNAMICS: T A U ..................... 41 3.1.1. GOVERNING EQUATIONS....................................... 41 3.1.2. SOLUTION M E TH O D ............................................. 45 3.2. CFD MESH G ENERATION................................................ 46 3.3. COMPUTATIONAL STRUCTURAL DYNAMICS: MSC NASTRAN 47 3.3.1. LINEAR GOVERNING EQUATIONS ........................... 48 3.3.2. MODAL A NALYSIS................................................ 48 3.3.3. GENERALISED EQUATIONS OF M O TIO N .................. 49 3.3.4. NONLINEAR SOLUTION M E TH O D ........................... 50 3.4. CFD MESH DEFORMATION: FSDEFORMATION .................. 51 3.4.1. RADIAL BASIS FUNCTION IN TERP O LATIO N ............ 51 3.4.2. BASIC ALGORITHM MESH DEFORMATION ............ 53 3.4.3. BASE POINT SELECTION....................................... 57 3.4.3.1. EQUIDISTANT REDUCTION METHOD . . . 57 3.4.3.2. ERROR C ORRECTION.............................. 58 3.4.3.3. DISTANCES WEIGHTING BY INTERPOLATION E R R O R ................................................ 59 3.4.3.4. INTERPOLATION QUALITY COMPARISON . 60 3.4.4. NEAREST NEIGHBOUR CORRECTION ........................ 63 3.5. CFD-CSM COUPLING: FSADVANCEDSPLINING ............... 64 3.5.1. COUPLING CONCEPT .......................................... 65 3.5.2. RELAXATION AND BLENDING................................. 66 3.5.3. INTERPOLATION M ETHODS .................................... 67 3.5.4. LOAD TRANSFER............................................. .. . 68 3.5.5. COUPLING E X AM P LE.......................................... 68 3.6. CFD-CSM IN TERACTIO N ................................................ 69 3.6.1. STEADY: FSNASTRANLNTHELOOP ..................... 69 3.6.2. UNSTEADY TIME-DOMAIN: F S S W IN G ............... 71 3.6.3. UNSTEADY AERODYNAMICS: FSFORCEDMOTION . . 72 3.6.4. UNSTEADY FREQUENCY DOMAIN: P-K-METHOD . . 73 3.7. FLOWSIMULATOR ............................................................ 75 4. ASPECTS OF UNSTEADY AERODYNAMIC EFFECTS FOR FLUTTER 77 4.1. INFLUENCE OF REDUCED FREQUENCY................................. 78 4.2. INFLUENCE OF STEADY AERODYNAMICS AND INVERSE SHOCK M OTION........................................................................... 79 4.3. COMPARISON OF CFD AND D L M ................................. 82 4.4. INFLUENCE OF MACH N UM BER.......................................... 83 4.5. INFLUENCE OF MOTION A M P LITU D E ................................. 85 4.6. TURBULENCE M O D ELLIN G ................................................ 86 5. DESCRIPTION OF AEROSTABIL EXPERIMENT 89 5.1. LIMIT-CYCLE OSCILLATION EXPERIMENT .................... 89 5.1.1. ANALYSIS AND COMPARISON TO SIMULATION . . . 92 5.1.2. MEASUREMENT A C C U RA C Y ................................. 93 5.2. FLIB EXPERIMENT......................................................... 93 6. COMPUTATIONAL MODELING 95 6.1. AERODYNAMICS............................................................... 95 6.1.1. CFD MESH CONVERGENCE S TU D IE S .................. 96 6.2. S TRU C TU R E ..................................................................... 97 7. STEADY FLUID-STRUCTURE INTERACTION ANALYSIS 101 7.1. COMPARISON STRUCTURAL BEAM VS. SHELL MODELLING . . 102 7.2. COMPARISON TO DEFORMATION MEASUREMENTS ................ 103 7.3. LIMIT-CYCLE FLOW C O N D ITIO N S........................................106 7.3.1. TURBULENCE M ODELLING........................................106 7.3.2. NONLINEAR S TR U C TU R E ...........................................109 7.3.3. CFD MESH CONVERGENCE.....................................I L L 7.4. QUASI-STEADY A NALYSIS ................................................... 112 8. DYNAMIC SINGLE DEGREE OF FREEDOM ANALYSIS 115 8.1. FLUTTER ANALYSIS .............................................................116 8.2. TIME-DOMAIN LCO ANALYSIS...........................................122 9. DYNAMIC MULTI DEGREE OF FREEDOM ANALYSIS 129 9.1. FLUTTER ANALYSIS ............................................................ 129 9.1.1. DEGREE OF FREEDOM CONVERGENCE ......................129 9.1.2. CFD MESH CONVERGENCE.....................................132 9.1.3. NONLINEAR STRUCTURAL M O D EL...............................133 9.1.4. DYNAMIC PRESSURE R A N G E ..................................135 9.2. TIME-DOMAIN LCO ANALYSIS...........................................140 9.2.1. COMPARISON TO EXPERIMENTS...............................140 9.2.2. LCO M ECHANISM .................................................145 9.3. STUDIES...............................................................................149 9.3.1. UNSTEADY INFLUENCE OF CAMBER BENDING . . . 149 9.3.2. INFLUENCE OF ANGLE OF A TTACK ...............................152 10. REFERENCE CASE 155 10.1. SIMULATION S E TU P ............................................................ 155 10.2. STEADY SOLUTION AND FLUTTER ANALYSIS............................157 10.3. LIMIT-CYCLE O SCILLATIONS.................................................158 10.4. HINTS FOR CASE-RECOMPUTATION........................................159 11. CONCLUSION 163 11.1. SUMMARY OF R E S U LTS ...................................................... 163 11.2. FUTURE WORK ...................................................................165 A. APPENDIX 167 A.L. FLOW PARAM ETER................................................................167 A.2. PULSE E X A M P LE ................................................................169 A.3. REYNOLDS STRESS M O D EL....................................................169 A.4. MODE SHAPES ON AERODYNAMIC S URFACE.........................171 A.5. 2-DOF LCO AMPLITUDES OF SENSOR 7 ............................172 A.6. UNSTEADY AERODYNAMICS AND WORK-PER-CYCLE SUP PLEMENT ........................................................................... 174 A.7. CFD PARAMETER FOR REFERENCE C ASE...............................175 A.8. AUTHOR CONTRIBUTIONS TO PUBLICATIONS 175
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series2	Forschungsbericht / DLR, Deutsches Zentrum für Luft- und Raumfahrt
spelling	Stickan, Bernd Verfasser (DE-588)1169778313 aut Explanation of AEROSTABIL limit-cycle oscillations via high-fidelity aeroelastic simulations Bernd Stickan Als Manuskript gedruckt Köln DLR, Deutsches Zentrum für Luft- und Raumfahrt 2018 188 Seiten Illustrationen, Diagramme 21 cm txt rdacontent n rdamedia nc rdacarrier Forschungsbericht / DLR, Deutsches Zentrum für Luft- und Raumfahrt 2018-23 Dissertation Universität Carolo-Wilhelmina zu Braunschweig 2018 Zusammenfassungen deutsch und englisch Transsonische Strömung (DE-588)4135633-0 gnd rswk-swf Schwingung (DE-588)4053999-4 gnd rswk-swf Flattern Technik (DE-588)4204298-7 gnd rswk-swf Computersimulation (DE-588)4148259-1 gnd rswk-swf Aerodynamik (DE-588)4000589-6 gnd rswk-swf Grenzzykel (DE-588)4158165-9 gnd rswk-swf Numerische Strömungssimulation (DE-588)4690080-9 gnd rswk-swf Fluid-Struktur-Wechselwirkung (DE-588)4314754-9 gnd rswk-swf Aeroelastizität (DE-588)4202469-9 gnd rswk-swf (DE-588)4113937-9 Hochschulschrift gnd-content Aerodynamik (DE-588)4000589-6 s Aeroelastizität (DE-588)4202469-9 s Transsonische Strömung (DE-588)4135633-0 s Grenzzykel (DE-588)4158165-9 s Schwingung (DE-588)4053999-4 s Flattern Technik (DE-588)4204298-7 s Fluid-Struktur-Wechselwirkung (DE-588)4314754-9 s Numerische Strömungssimulation (DE-588)4690080-9 s Computersimulation (DE-588)4148259-1 s DE-604 DLR, Deutsches Zentrum für Luft- und Raumfahrt Forschungsbericht 2018-23 (DE-604)BV011758990 2018,23 B:DE-101 application/pdf http://d-nb.info/1172732329/04 Inhaltsverzeichnis DNB Datenaustausch application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=030782912&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis
spellingShingle	Stickan, Bernd Explanation of AEROSTABIL limit-cycle oscillations via high-fidelity aeroelastic simulations DLR, Deutsches Zentrum für Luft- und Raumfahrt Forschungsbericht Transsonische Strömung (DE-588)4135633-0 gnd Schwingung (DE-588)4053999-4 gnd Flattern Technik (DE-588)4204298-7 gnd Computersimulation (DE-588)4148259-1 gnd Aerodynamik (DE-588)4000589-6 gnd Grenzzykel (DE-588)4158165-9 gnd Numerische Strömungssimulation (DE-588)4690080-9 gnd Fluid-Struktur-Wechselwirkung (DE-588)4314754-9 gnd Aeroelastizität (DE-588)4202469-9 gnd
subject_GND	(DE-588)4135633-0 (DE-588)4053999-4 (DE-588)4204298-7 (DE-588)4148259-1 (DE-588)4000589-6 (DE-588)4158165-9 (DE-588)4690080-9 (DE-588)4314754-9 (DE-588)4202469-9 (DE-588)4113937-9
title	Explanation of AEROSTABIL limit-cycle oscillations via high-fidelity aeroelastic simulations
title_auth	Explanation of AEROSTABIL limit-cycle oscillations via high-fidelity aeroelastic simulations
title_exact_search	Explanation of AEROSTABIL limit-cycle oscillations via high-fidelity aeroelastic simulations
title_full	Explanation of AEROSTABIL limit-cycle oscillations via high-fidelity aeroelastic simulations Bernd Stickan
title_fullStr	Explanation of AEROSTABIL limit-cycle oscillations via high-fidelity aeroelastic simulations Bernd Stickan
title_full_unstemmed	Explanation of AEROSTABIL limit-cycle oscillations via high-fidelity aeroelastic simulations Bernd Stickan
title_short	Explanation of AEROSTABIL limit-cycle oscillations via high-fidelity aeroelastic simulations
title_sort	explanation of aerostabil limit cycle oscillations via high fidelity aeroelastic simulations
topic	Transsonische Strömung (DE-588)4135633-0 gnd Schwingung (DE-588)4053999-4 gnd Flattern Technik (DE-588)4204298-7 gnd Computersimulation (DE-588)4148259-1 gnd Aerodynamik (DE-588)4000589-6 gnd Grenzzykel (DE-588)4158165-9 gnd Numerische Strömungssimulation (DE-588)4690080-9 gnd Fluid-Struktur-Wechselwirkung (DE-588)4314754-9 gnd Aeroelastizität (DE-588)4202469-9 gnd
topic_facet	Transsonische Strömung Schwingung Flattern Technik Computersimulation Aerodynamik Grenzzykel Numerische Strömungssimulation Fluid-Struktur-Wechselwirkung Aeroelastizität Hochschulschrift
url	http://d-nb.info/1172732329/04 http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=030782912&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA
volume_link	(DE-604)BV011758990
work_keys_str_mv	AT stickanbernd explanationofaerostabillimitcycleoscillationsviahighfidelityaeroelasticsimulations

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