Hypersonic orbiter separation from a carrier:
Gespeichert in:
| 1. Verfasser: | |
|---|---|
| Format: | Abschlussarbeit Buch |
| Sprache: | English |
| Veröffentlicht: |
2012
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| Schlagworte: | |
| Online-Zugang: | Volltext https://nbn-resolving.org/urn:nbn:de:bvb:91-diss-20121008-1092612-0-4 Inhaltsverzeichnis |
| Beschreibung: | XII, 174 S. Ill., graph. Darst. |
Internformat
MARC
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| 300 | |a XII, 174 S. |b Ill., graph. Darst. | ||
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| 502 | |a München, Techn. Univ., Diss., 2012 | ||
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Datensatz im Suchindex
| _version_ | 1804150170824212480 |
|---|---|
| adam_text | IMAGE 1
LIST OF CONTENTS
NOMENCLATURES VIII
1 INTRODUCTION 1
1.1 BACKGROUND O F SPACE TRANSPORTATION AND SEPARATION PROCESS 1
1.2 FEATURES OF THE HYPERSONIC FLIGHT AND ITS RESEARCH METHODS 4
1.3 RELEVANT RESEARCH WORKS 5
1.4 THESIS OUTLINE 6
2 PHYSICAL AND MATHEMATICAL MODELS 8
2.1 GEOMETRY MODELS AND FLUID ASSUMPTIONS 8
2.2 NAVIER-STOKES AND EULER EQUATION SYSTEMS 9
2.3 TURBULENCE MODEL 13 L
2.4 BOUNDARY AND INITIAL CONDITIONS 15
3 NUMERICAL METHOD 18
3.1 BASIC COORDINATE TRANSFORMATION 18
3.2 DISCRETIZATION IN TIME AND SPACE ^ 20
3.3 MODIFIED AUSM AND MUSCL SCHEMES FOR INVISCID TERMS 23
3.3.1 MODIFIED AUSM SCHEME 23
3.3.2 MUSCL SCHEME 27
3.4 CHAKRAVARTHY SCHEME FOR VISCOUS TERMS 28
4 COMPUTATIONAL MESH 31
4.1 MESHING METHODS 31
4.2 BASIC GEOMETRY AND INITIAL MESH 32
4.3 ORTHOGONALIZATION AND SMOOTHNESS 33
5 EXPERIMENTS AND MEASUREMENT TECHNIQUES 36
5.1 WIND TUNNEL T-313 AND ITS SET-UP 36
HTTP://D-NB.INFO/1033002321
IMAGE 2
5.2 SHOCK TUNNEL TH2-D AND ITS SET-UP 41
6 NUMERICAL RESULTS CORRESPONDING TO THE EXPERIMENTS OF ITAM 46
6.1 STEADY INVISCID AND LAMINAR FLOWS 46
6.2 UNSTEADY INVISCID AND LAMINAR FLOWS 55
6.2.1 PITCHING MOVEMENT IN INVISCID FLOW 56
6.2.2 TRANSLATION IN INVISCID FLOW 58
6.2.3 SEPARATION PROCESS IN INVISCID FLOW 59
6.2.4 SEPARATION PROCESS IN LAMINAR FLOW 63
6.3 FREE ORBITAL STAGE AT = 4.05 65
6.4 INFLUENCE OF TURBULENT FLOW 66
7 NUMERICAL RESULTS CORRESPONDING TO THE EXPERIMENTS OF RWTH 70
7.1 COMPARISON BETWEEN M_ = 4.05 AND = 7.9 70
7.2 PRESSURE DISTRIBUTION FOR H/L = 0.1812 72
7.3 PRESSURE DISTRIBUTION FOR H/L = 0.0812 75
7.4 PRESSURE DISTRIBUTION FOR H/L = 0.0662 77
7.5 AERODYNAMIC COEFFICIENT COMPARISONS 80
7.6 FREE ORBITAL STAGE AT = 7.9 81
8 PREDICTION OF THE AERODYNAMIC PROPERTIES AT MACH 6.8 83
8.1 SHOCK STRUCTURE ANALYSIS 83
8.1.1 STRUCTURE OF EOS BOW SHOCK 83
8.1.2 SHOCK STRUCTURES DEPENDENT ON DISTANCES BETWEEN THE TWO STAGES 87
8.1.3 SHOCK STRUCTURES DEPENDENT ON MACH NUMBERS 92
8.1.4 SHOCK STRUCTURES DEPENDENT ON ANGLES OF ATTACK 93
8.1.5 SHOCK STRUCTURES ON 3D EOS SURFACE 95
8.2 PRESSURE COEFFICIENTS RELATED TO SHOCK STRUCTURES 98
IMAGE 3
8.3 AERODYNAMIC COEFFICIENTS 107
8.4 COMPARISON WITH MACH 4.05 IN DESIGNED ENVIRONMENT 110
8.5 TURBULENCE SIMULATION 112
8.6 UNSTEADY SEPARATION PROCESS 113
9 CONCLUSION 119
REFERENCES 122
APPENDICES 133
A VECTOR OPERATION 133
B CONSERVATION EQUATIONS 135
B.L MASS CONSERVATION EQUATIONS 135
B.2 MOMENTUM CONSERVATION EQUATIONS 136
B.3 ENERGY CONSERVATION EQUATIONS 137
C NAVIER-STOKES EQUATIONS 139
C.L STRESS TENSOR 139
C.2 SYMMETRICAL STRESS MATRIX 140
C.3 NAVIER-STOKES AND EULER EQUATIONS 141
D NONDIMENSIONLIZATION 145
E CURVILINEAR TRANSFORMATION 148
E.L COORDINATE TRANSFORMATION 148
E.2 DIMENSIONLESS AND CURVILINEAR NS EQUATIONS 149
F QUASI-LINEAR EULER EQUATIONS 153
G INITIAL AND BOUNDARY CONDITIONS 155
G1 CHARACTERISTIC VARIABLES 155
G 2 BOUNDARY CONDITIONS FOR INFLOW AND OUTFLOW 157
IMAGE 4
G3 EULER IMPERMEABLE BOUNDARY CONDITIONS 160
G 4 NAVIER-STOKES IMPERMEABLE BOUNDARY CONDITIONS 161
G5 SYMMETRIC BOUNDARY CONDITIONS 162
H BALDWIN-LOMAX TURBULENCE MODEL 163
I DIMENSIONLESS AERODYNAMIC COEFFICIENTS 166
J CHARACTERISTICS OF THE HVNERSONIC FLOW 168
K STANDARD ATMOSPHERE PROPERTIES 169
K.L US STANDARD ATMOSPHERE 1976 169
K.2 FORTRAN PROGRAM FOR STANDARD ATMOSPHERE 171
L REAL GAS EFFECT 174
|
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| spelling | Jiang, Lei Verfasser aut Hypersonic orbiter separation from a carrier Lei Jiang 2012 XII, 174 S. Ill., graph. Darst. txt rdacontent n rdamedia nc rdacarrier München, Techn. Univ., Diss., 2012 (DE-588)4113937-9 Hochschulschrift gnd-content Erscheint auch als Online-Ausgabe urn:nbn:de:bvb:91-diss-20121008-1092612-0-4 http://mediatum.ub.tum.de/node?id=1092612 Verlag kostenfrei Volltext https://nbn-resolving.org/urn:nbn:de:bvb:91-diss-20121008-1092612-0-4 Resolving-System DNB Datenaustausch application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=025868855&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
| spellingShingle | Jiang, Lei Hypersonic orbiter separation from a carrier |
| subject_GND | (DE-588)4113937-9 |
| title | Hypersonic orbiter separation from a carrier |
| title_auth | Hypersonic orbiter separation from a carrier |
| title_exact_search | Hypersonic orbiter separation from a carrier |
| title_full | Hypersonic orbiter separation from a carrier Lei Jiang |
| title_fullStr | Hypersonic orbiter separation from a carrier Lei Jiang |
| title_full_unstemmed | Hypersonic orbiter separation from a carrier Lei Jiang |
| title_short | Hypersonic orbiter separation from a carrier |
| title_sort | hypersonic orbiter separation from a carrier |
| topic_facet | Hochschulschrift |
| url | http://mediatum.ub.tum.de/node?id=1092612 https://nbn-resolving.org/urn:nbn:de:bvb:91-diss-20121008-1092612-0-4 http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=025868855&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
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