Holdings: Wake vortices of landing aircraft

Wake vortices of landing aircraft:

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Bibliographic Details
Main Author:	Stephan, Anton (Author)
Format:	Thesis Book
Language:	English
Published:	Köln DLR 2013 [erschienen] 2014
Edition:	Als Ms. gedr.
Series:	Forschungsbericht / Deutsches Zentrum für Luft- und Raumfahrt 2014,10
Subjects:	Landung LES > Strömung Wirbelschleppe Hochschulschrift
Online Access:	Inhaltsverzeichnis
Physical Description:	XIII, 148 S. Ill., zahlr. graph. Darst.

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MARC


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adam_text	INHALTSVERZEICHNIS ABSTRACT VI ZUSAMMENFASSUNG IX 1. INTRODUCTION 1 1.1. MOTIVATION . . . 1 1.2. AINIS OF THE THESIS 2 1.3. STATC-OF-THE-ART - REEENT DEVELOPMENTS 7 1.4. OVERVIEW OVEI THE THESIS 10 2. METHODS 13 2.1. WAKE-VORTEX PRINCIPLES 13 2 11 WAKE-VORTEX AND HFT GENERATION OF AN AIRCRAFT . . 13 2.1.2. WING IN GRONND EFFEET . . . . . IG 2 1.3. PLIASES OF WAKE-VORTEX EVOLUTION .... . . 17 2 1.4. LANDING PLIASES . . . . . . 19 2.1.5 FLIGHT, TEST DATA . ... . 21 2.1 6 VORTEX INODELS AND PARANIETERS 23 2.2. AMBIENT TURBULENCE FIELD 28 2.2.1. AMBIENT WIND . . 28 2.2 2. STRNT WAKE TURBULENCE 30 2.3. LES CODE ... 32 2.3.1. GOVERNING EQUATIONS 33 2.3.2. LAGRANGIAN DYNAMIC SUBGND-SEALE NIODEL . . 34 2.3.3 FOURTH-ORDER FINITE VOLNNIE COMPACT SCHERNE . . 30 2.3.4. SPLIT-INTERFAEE ALGONTHM .... 37 2.3.5. VELOCITY-PRESSURE ITERATION METHOD ON A MULTI GRID 37 2.3.6. THIRD-ORDER RUNGE-KUTTA 38 2.3.7. OBSTAELE MODELING . . 39 2 4. LES OF BOUNDARY LAYER FLOW 39 2 4.1. RESOLUTION REQUIREMENTS AND CORNPUTATIONAL COMPLEXITY 40 2 4.2. WALL NIODEL FOR THE GROUND SURFACE 41 2.5. RANS/LES COTIPLING 42 2.5.1. FORTIFIED SOLUTION ALGORITHM 43 2.5 2. RANS/LES INTCRFACC 44 HTTP://D-NB.INFO/1049989872 XII INHALTSVERZEICHNIS 2.5 3. ALICRA.FT DESCENT AND TOUCHDOWN . 45 2.5 4. BOUNDARY TREATMCNT . . . 47 2.6. TURBULENCE INITIALIZATION . . . . 47 2.6.1. WIND INITIALIZATION 47 2.6 2 STRUT WAKE INITIALIZATION . . . 48 2.7. WAKE-VORTEX INITIALIZATION 50 2.7.1. TEMPORAL LES 50 2.7 2. SPATIAL LES 51 2.7.3. HANS FLOW IICLD * . . 51 2 8 COMPUTATIONAL DOMAIN 52 2.8.1. TEMPORAL LES . . 52 2.8.2. SPATIAL LES 53 2.9. POST-PIOCESSMG .... 54 2.9.1. VORTEX CENTER TRACKING 54 2.9.2. SECONDARY VORTEX LIELIX ... 55 3. RESULTS 57 3.1. LISTING OF SIINULATIONS . . 57 3.2. FLOW FIELD OF A LANDING AIICRAFT ... 59 3.2 1. CONIPLETE LANDING 59 3.2 2. VOITCX PAIR M GROUND PROXNNITY 62 3.2.3. CROSSWIND EFFECT .... 62 3.2.4. OBSTACLE EFFECT . . . 63 3.3. WAKE-VORTEX EVOLUTION WITH FIAT GROUND 65 3.3.1. IN GROUND EFFECT WITHOUT TURBULENCE. ACADEMIC CASE . . 65 3.3.2. WAKE -VORTEX DECAY MECHAIIISNIS IN CROSSWIND SITUATION . . . . 65 3 3.3. TRAJECTORIES AND DECAY . . . . 69 3 3.4. THE EFFECT OF A WALL INODEL IN LIIGLI REYNOLDS NUNIBER FIOWS 71 3.4. OBSTACLE EFFECTS 73 3.4.1. DETAILCD ANALYSIS OF VORTEX DYNAMICS WITLI OBSTACLE . 73 3.4 2. TRAJECTORIES AND DECAY 79 3.4.3. EFFECTS OF DIFFERENT OBSTACLE GEOMETRIES AND LIEADWIND 80 3.5. WMG-IN-GROUND EFFECT 84 3.6. TOUCHDOWN EFFECTS 86 3 6.1. VORTEX DIVCRGENCE . 86 3.6.2. END CFFECTS ... ... 86 3.7. WAKE VORTEX TOPOLOGY ... 89 3.8. VORTEX DECAY AND COIE RADIUS EVOLUTION 89 3.8.1. FIAT GROUND 89 3.8.2. PLATE LINE EFFEETS 91 3.8.3. WAKE-VORTEX DECAY PHASES IN GROUND PROXINUTY 93 4. DISCUSSION 95 INHALTSVERZEICHNIS XIII 4.1. COMPANSON OF LES WITLI TOWING TANK EXPERIMENTS 95 4.1.1. EXPERIMCNTAL SETNP - WATER TOWING TANK .... . .... 95 4.1.2. NNMERICAL SETNP 90 4.1.3. SIMULATION . . . 90 4 1.4. EXPERIMENT . . . 98 4 1.5. TRAJECTORIES AND DCCAY 100 4 1.0. PROPAGATION OF END EFFEETS . ... . 104 4.1.7. EFFEETS OF SEVERAL OBSTAELES 104 4.2. COMPARISON WITH FIELE! INCASUREMENT CAMPAIGNS 107 4.2.1. FRANKFURT (WAKEFRA) 108 4.2.2. MUNICH (WFCKCMUC) 108 4.3. GENERAL REMARKS . 114 5. CONCLUSIONS AND OUTLOOK 115 A. APPENDIX: AIRCRAFT GEOMETRY 119 B. APPENDIX: ROUGH SURFACES 123 NOMENCLATURE 125 ABBILDUNGSVERZEICHNIS 131 TABELLENVERZEICHNIS 135 LITERATURVERZEICHNIS 137 ACKNOWLEDGMENTS 148
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indexdate	2024-07-10T01:05:50Z
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language	English
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physical	XIII, 148 S. Ill., zahlr. graph. Darst.
publishDate	2013
publishDateSearch	2014
publishDateSort	2014
publisher	DLR
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series2	Forschungsbericht / Deutsches Zentrum für Luft- und Raumfahrt
spelling	Stephan, Anton Verfasser aut Wake vortices of landing aircraft Anton Stephan Als Ms. gedr. Köln DLR 2013 [erschienen] 2014 XIII, 148 S. Ill., zahlr. graph. Darst. txt rdacontent n rdamedia nc rdacarrier Forschungsbericht / Deutsches Zentrum für Luft- und Raumfahrt 2014,10 Zugl.: München, Univ., Diss., 2014 Landung (DE-588)4120649-6 gnd rswk-swf LES Strömung (DE-588)4315616-2 gnd rswk-swf Wirbelschleppe (DE-588)4384015-2 gnd rswk-swf (DE-588)4113937-9 Hochschulschrift gnd-content Landung (DE-588)4120649-6 s Wirbelschleppe (DE-588)4384015-2 s LES Strömung (DE-588)4315616-2 s DE-604 Deutsches Zentrum für Luft- und Raumfahrt Forschungsbericht 2014,10 (DE-604)BV011758990 2014,10 DNB Datenaustausch application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=027253150&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis
spellingShingle	Stephan, Anton Wake vortices of landing aircraft Landung (DE-588)4120649-6 gnd LES Strömung (DE-588)4315616-2 gnd Wirbelschleppe (DE-588)4384015-2 gnd
subject_GND	(DE-588)4120649-6 (DE-588)4315616-2 (DE-588)4384015-2 (DE-588)4113937-9
title	Wake vortices of landing aircraft
title_auth	Wake vortices of landing aircraft
title_exact_search	Wake vortices of landing aircraft
title_full	Wake vortices of landing aircraft Anton Stephan
title_fullStr	Wake vortices of landing aircraft Anton Stephan
title_full_unstemmed	Wake vortices of landing aircraft Anton Stephan
title_short	Wake vortices of landing aircraft
title_sort	wake vortices of landing aircraft
topic	Landung (DE-588)4120649-6 gnd LES Strömung (DE-588)4315616-2 gnd Wirbelschleppe (DE-588)4384015-2 gnd
topic_facet	Landung LES Strömung Wirbelschleppe Hochschulschrift
url	http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=027253150&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA
volume_link	(DE-604)BV011758990
work_keys_str_mv	AT stephananton wakevorticesoflandingaircraft

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