Numerical analysis of transition effects for SCRamjet intake flows:
Gespeichert in:
1. Verfasser: | |
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Format: | Abschlussarbeit Buch |
Sprache: | English |
Veröffentlicht: |
Aachen
Shaker
2010
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Schriftenreihe: | Berichte aus der Luft- und Raumfahrttechnik
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Schlagworte: | |
Online-Zugang: | Inhaltsverzeichnis |
Beschreibung: | XII, 158 S. Ill., graph. Darst. |
ISBN: | 9783832292164 |
Internformat
MARC
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245 | 1 | 0 | |a Numerical analysis of transition effects for SCRamjet intake flows |c Martin Krause |
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Datensatz im Suchindex
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adam_text | CONTENTS 1 INTRODUCTION 1 2 HYPERSONIC FLOW PHENOMENA AND LITERATURE
REVIEW 7 2.1 HYPERSONIC FLOW PHENOMENA 7 2.2 INTERNATIONAL SCRAMJET
RESEARCH IN THE PAST DECADES 14 2.3 SCRAMJET INTAKE DESIGN ISSUES 17 2.4
TRANSITION 22 2.4.1 NATURAL TRANSITION 22 2.4.2 BY-PASS TRANSITION 24
2.4.3 SEPARATED FLOW TRANSITION 25 2.4.4 WAKE INDUCED TRANSITION 26
2.4.5 SHOCK INDUCED SEPARATION AND TRANSITION 26 2.4.6 GOERTIER VORTICES
27 2.4.7 REVERSE TRANSITION OR RELARNINARISATION 28 2.4.8 INFLUENCE OF
HYPERSONIC FLOW VELOCITY ON TRANSITION PHENOMENA . . 29 2.5 TRANSITION
PREDICTION 30 2.5.1 DIRECT NUMERICAL SIMULATION (DNS) 30 2.5.2 LARGE
EDDY SIMULATION (LES) 31 2.5.3 LOCAL STABILITY METHOD (E N -METHOD) 32
2.5.4 EMPIRICAL CORRELATIONS FOR TRANSITION ONSET 33 2.5.5 THE AUTHOR S
CHOICE FOR TRANSITION PREDICTION 34 3 GOVERNING EQUATIONS 37 3.1
CONSERVATION LAWS 37 3.2 CONSTITUTIVE EQUATIONS OF PERFECT VISCOUS GASES
38 3.3 THE CLOSURE PROBLEM OF TURBULENCE MODELLING 41 3.3.1 TIME
AVERAGING TECHNIQUES 42 3.3.2 THE CLOSURE APPROACHES 43 3.4 TURBULENCE
MODELS 44 3.4.1 THE SHEAR STRESS TRANSPORT MODEL (SST) OF MENTER 45 3.5
TRANSITION MODELS 47 3.5.1 WALTERS AND LEYLEK TRANSITION MODEL [142,143]
48 3.5.2 TRANSITION MODEL BY WARREN AND HASSAN [144,145] 49 3.5.3
TRANSITION MODE BIBLIOGRAFISCHE INFORMATIONEN
HTTP://D-NB.INFO/1004936346 DIGITALISIERT DURCH CONTENTS 3.5.4
CONDITIONED AVERAGED NAVIER-STOKES EQUATION TRANSITION MODEL BY STEELANT
AND DICK [124,125] 50 3.5.5 TRANSITION MODEL BY SUZEN AND HUANG
[130-132] 51 3.5.6 TRANSITION MODEL BY MENTER AND LANGTRY [69,70,83] 51
4 NUMERICAL METHOD 59 4.1 FLOWERCODE 59 4.2 QUADFLOWCODE 60 4.3 FINITE
VOLUME METHOD 61 4.4 SPATIAL DISCRETISATION 63 4.5 TIME INTEGRATION 64
4.6 GRID GENERATION 65 4.7 FAR-FIELD BOUNDARY CONDITIONS 65 5 NUMERICAL
ASPECTS AND DEVELOPMENT OF THE TRANSITION CORRELATIONS 69 5.1
DEVELOPMENT OF THE TRANSITION CORRELATIONS 69 5.1.1 TRANSITION
CORRELATIONS FOR SUBSONIC FLOW 70 5.1.2 TRANSITION CORRELATIONS FOR
SUPERSONIC FLOW 73 5.2 INFLUENCE OF THE NUMERICAL GRID ON THE TRANSITION
BEHAVIOUR 75 5.2.1 GRID CONVERGENCE STUDY: THE INFLUENCE OF GRID DENSITY
77 5.2.2 GRID CONVERGENCE STUDY: THE INFLUENCE OF Y + 77 5.2.3 GRID
CONVERGENCE STUDY: THE INFLUENCE OF DISTANCE BETWEEN FARFIELD BOUNDARY
AND LEADING EDGE 79 5.3 CALIBRATION OF THE CORRELATIONS FOR HYPERSONIC
TEST CASES 82 6 RESULTS 85 6.1 FLATPLATEFLOW 85 6.1.1 SUBSONIC FLAT
PLATE TEST CASES 85 6.1.2 HYPERSONIC FLAT PLATE TEST CASES 86 6.2
HYPERSONIC RAMP FLOW 90 6.2.1 HYPERSONIC SINGLE RAMP 90 6.2.2 HYPERSONIC
DOUBLE RAMP 93 6.3 EXPERIMENTALLY EXAMINED SCRAMJET INTAKE FLOWS 102
6.3. CONTENTS A BEST PRACTICE GUIDELINES 145 BIBLIOGRAPHY 147
|
any_adam_object | 1 |
author | Krause, Martin 1980- |
author_GND | (DE-588)14193770X |
author_facet | Krause, Martin 1980- |
author_role | aut |
author_sort | Krause, Martin 1980- |
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building | Verbundindex |
bvnumber | BV036791827 |
ctrlnum | (OCoLC)671353899 (DE-599)DNB1004936346 |
dewey-full | 629.1343535 |
dewey-hundreds | 600 - Technology (Applied sciences) |
dewey-ones | 629 - Other branches of engineering |
dewey-raw | 629.1343535 |
dewey-search | 629.1343535 |
dewey-sort | 3629.1343535 |
dewey-tens | 620 - Engineering and allied operations |
discipline | Maschinenbau / Maschinenwesen Verkehr / Transport |
format | Thesis Book |
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id | DE-604.BV036791827 |
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indexdate | 2024-07-09T22:48:12Z |
institution | BVB |
isbn | 9783832292164 |
language | English |
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physical | XII, 158 S. Ill., graph. Darst. |
publishDate | 2010 |
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publisher | Shaker |
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series2 | Berichte aus der Luft- und Raumfahrttechnik |
spelling | Krause, Martin 1980- Verfasser (DE-588)14193770X aut Numerical analysis of transition effects for SCRamjet intake flows Martin Krause Aachen Shaker 2010 XII, 158 S. Ill., graph. Darst. txt rdacontent n rdamedia nc rdacarrier Berichte aus der Luft- und Raumfahrttechnik Zugl.: Aachen, Techn. Hochsch., Diss., 2010 Grenzschichtumschlag (DE-588)4763105-3 gnd rswk-swf Numerisches Verfahren (DE-588)4128130-5 gnd rswk-swf Überschallstaustrahltriebwerk (DE-588)4427457-9 gnd rswk-swf (DE-588)4113937-9 Hochschulschrift gnd-content Überschallstaustrahltriebwerk (DE-588)4427457-9 s Grenzschichtumschlag (DE-588)4763105-3 s Numerisches Verfahren (DE-588)4128130-5 s DE-604 DNB Datenaustausch application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=020708216&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
spellingShingle | Krause, Martin 1980- Numerical analysis of transition effects for SCRamjet intake flows Grenzschichtumschlag (DE-588)4763105-3 gnd Numerisches Verfahren (DE-588)4128130-5 gnd Überschallstaustrahltriebwerk (DE-588)4427457-9 gnd |
subject_GND | (DE-588)4763105-3 (DE-588)4128130-5 (DE-588)4427457-9 (DE-588)4113937-9 |
title | Numerical analysis of transition effects for SCRamjet intake flows |
title_auth | Numerical analysis of transition effects for SCRamjet intake flows |
title_exact_search | Numerical analysis of transition effects for SCRamjet intake flows |
title_full | Numerical analysis of transition effects for SCRamjet intake flows Martin Krause |
title_fullStr | Numerical analysis of transition effects for SCRamjet intake flows Martin Krause |
title_full_unstemmed | Numerical analysis of transition effects for SCRamjet intake flows Martin Krause |
title_short | Numerical analysis of transition effects for SCRamjet intake flows |
title_sort | numerical analysis of transition effects for scramjet intake flows |
topic | Grenzschichtumschlag (DE-588)4763105-3 gnd Numerisches Verfahren (DE-588)4128130-5 gnd Überschallstaustrahltriebwerk (DE-588)4427457-9 gnd |
topic_facet | Grenzschichtumschlag Numerisches Verfahren Überschallstaustrahltriebwerk Hochschulschrift |
url | http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=020708216&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
work_keys_str_mv | AT krausemartin numericalanalysisoftransitioneffectsforscramjetintakeflows |