Selected aerothermodynamic design problems of hypersonic flight vehicles:
Gespeichert in:
| Beteiligte Personen: | , |
|---|---|
| Format: | Buch |
| Sprache: | Englisch |
| Veröffentlicht: |
Berlin [u.a.]
Springer
2009
|
| Schlagwörter: | |
| Links: | http://deposit.dnb.de/cgi-bin/dokserv?id=3173859&prov=M&dok_var=1&dok_ext=htm http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=018014232&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
| Umfang: | XV, 518 S. Ill., graph. Darst. |
| ISBN: | 9783540899730 |
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| adam_text | REFERENCES 55 TABLE OF CONTENTS 1 INTRODUCTION 1 1.1 THREE REFERENCE
CLASSES OF HYPERSONIC VEHICLES 2 1.2 AEROTHERMODYNAMICS AND THE
DEFINITION AND DEVELOPMENT OF FLIGHT VEHICLES 4 1.2.1 DESIGN
SENSITIVITIES AND MARGINS VERSUS DATA UNCERTAINTIES 4 1.2.2 DEFICITS OF
AEROTHERMODYNAMIC SIMULATION MEANS .... 5 1.3 SCOPE AND CONTENT OF THE
BOOK 8 REFERENCES 9 2 SHORT INTRODUCTION TO FLIGHT TRAJECTORIES FOR
AEROTHERMODYNAMICISTS 11 2.1 FLIGHT TRAJECTORIES OF WINGED AND
NON-WINGED RE-ENTRY VEHICLES 13 2.1.1 GENERAL ASPECTS 13 2.1.2 GUIDANCE
OBJECTIVES, TRAJECTORY CONTROL VARIABLES, AND SYSTEMS AND OPERATIONAL
CONSTRAINTS 16 2.1.3 FORCES ACTING ON A RE-ENTRY VEHICLE 21 2.1.4 THE
EQUILIBRIUM GLIDE TRAJECTORY 24 2.1.5 EQUILIBRIUM GLIDE TRAJECTORY:
QUALITATIVE RESULTS .... 27 2.1.6 CASE STUDY 1: TRAJECTORIES OF RV-NW S
32 2.1.7 CASE STUDY 2: TRAJECTORY OF A RV-W (X-38) 34 2.2 FLIGHT
TRAJECTORIES OF CRUISE AND ACCELERATION VEHICLES 37 2.2.1 GENERAL
ASPECTS 37 2.2.2 GUIDANCE OBJECTIVES, TRAJECTORY CONTROL VARIABLES, AND
SYSTEMS AND OPERATIONAL CONSTRAINTS 40 2.2.3 FORCES ACTING ON A CRUISE
AND ACCELERATION VEHICLE ... 42 2.2.4 CASE STUDY 3: TRAJECTORY OF A CAV
(SAENGER) 44 2.3 GENERAL EQUATIONS FOR PLANETARY FLIGHT 47 2.4 PROBLEMS
54 BIBLIOGRAFISCHE INFORMATIONEN HTTP://D-NB.INFO/991138775
DIGITALISIERT DURCH X TABLE OF CONTENTS 3 AEROTHERMODYNAMIC DESIGN
PROBLEMS OF WINGED RE-ENTRY VEHICLES 59 3.1 OVERVIEW OF
AEROTHERMODYNAMIC ISSUES OF WINGED RE-ENTRY VEHICLES 59 3.1.1
AEROTHERMODYNAMIC PHENOMENA 59 3.1.2 MAJOR SIMULATION PROBLEM: HIGH MACH
NUMBER AND TOTAL ENTHALPY EFFECTS 64 3.2 PARTICULAR TRENDS IN RV-W
AEROTHERMODYNAMICS 64 3.2.1 STAGNATION PRESSURE 64 3.2.2 TOPOLOGY OF THE
WINDWARD SIDE VELOCITY FIELD 67 3.2.3 LIFT GENERATION 71 3.2.4 BASE
PRESSURE AND DRAG 73 3.3 AERODYNAMIC PERFORMANCE DATA OF RV-W S 74 3.3.1
SPACE SHUTTLE ORBITER 75 3.3.2 HERMES CONFIGURATION 78 3.3.3 HOPE-X
CONFIGURATION 81 3.3.4 X-34 CONFIGURATION 82 3.3.5 X-38 CONFIGURATION 85
3.3.6 HOPPER/PHOENIX CONFIGURATION 89 3.3.7 SUMMARY 91 3.4 VEHICLE
FLYABILITY AND CONTROLLABILITY 94 3.4.1 GENERAL CONSIDERATIONS 94 3.4.2
TRIM AND STABILITY OF RV-W S 95 3.5 THE HYPERSONIC PITCHING MOMENT
ANOMALY OF THE SPACE SHUTTLE ORBITER 98 3.5.1 TRIM SITUATION AND
POSSIBLE CAUSES OF THE PITCHING MOMENT ANOMALY 99 3.5.2 PRESSURE
COEFFICIENT DISTRIBUTION AT THE WINDWARD SIDE OF THE ORBITER 101 3.5.3
THE FORWARD SHIFT OF THE CENTER-OF-PRESSURE 107 3.6 THE HYPERSONIC
PITCHING MOMENT ANOMALY IN VIEW OF OSWATITSCH S MACH NUMBER INDEPENDENCE
PRINCIPLE 109 3.6.1 INTRODUCTION 109 3.6.2 WALL PRESSURE COEFFICIENT
DISTRIBUTION ILL 3.6. TABLE OF CONTENTS XI 4 AEROTHERMODYNAMIC DESIGN
PROBLEMS OF WINGED AIRBREATHING VEHICLES 129 4.1 OVERVIEW OF
AEROTHERMODYNAMIC ISSUES OF CRUISE AND ACCELERATION VEHICLES 130 4.1.1
AEROTHERMODYNAMIC PHENOMENA 130 4.1.2 MAJOR SIMULATION PROBLEM: VISCOUS
EFFECTS 137 4.2 PARTICULAR TRENDS IN CAV/ARV AEROTHERMODYNAMICS 141
4.2.1 STAGNATION PRESSURE 141 4.2.2 TOPOLOGY OF THE FOREBODY WINDWARD
SIDE VELOCITY FIELD 142 4.2.3 LIFT GENERATION 142 4.2.4 BASE PRESSURE
AND DRAG 142 4.2.5 AERODYNAMIC PERFORMANCE 144 4.3 EXAMPLE: FLIGHT
PARAMETERS AND AERODYNAMIC COEFFICIENTS OF THE REFERENCE CONCEPT SAENGER
145 4.4 GENERAL CONFIGURATIONAL ASPECTS: HIGHLY COUPLED LIFT AND
PROPULSION SYSTEM 153 4.4.1 SOME VEHICLE SHAPE CONSIDERATIONS 153 4.4.2
BOOKKEEPING OF AEROTHERMODYNAMIC AND PROPULSION SYSTEM FORCES 156 4.5
ISSUES OF AEROTHERMODYNAMIC AIRFRAME/PROPULSION INTEGRATION 164 4.5.1
FOREBODY EFFECT 165 4.5.2 FLAT VERSUS CONICAL LOWER SIDE OF FOREBODY 166
4.5.3 PRINCIPLE OF FOREBODY PRE-COMPRESSION 168 4.5.4 NET THRUST
SENSITIVITY ON PRE-COMPRESSION 172 4.5.5 INLET RAMP FLOW 175 4.6
WAVERIDER CONFIGURATIONS 179 4.6.1 INTRODUCTION 179 4.6.2 DESIGN METHODS
180 4.6.3 EXEMPLARY WAVERIDER DESIGNS 185 4.6.4 INFLUENCE OF VISCOUS
EFFECTS ON THE AERODYNAMIC PERFORMANCE 188 4.6.5 OFF-DESIGN AND
LOW-SPEED BEHAVIOR 192 4.6. XII TABLE OF CONTENTS 5.2 GENERAL
CONFIGURATIONAL ASPECTS 215 5.2.1 BALLISTIC PROBES 215 5.2.2 LIFTING
CAPSULES 218 5.2.3 BICONES 222 5.3 TRIM CONDITIONS AND STATIC STABILITY
OF RV-NW S 224 5.3.1 PARK S FORMULA 224 5.3.2 PERFORMANCE DATA OF
LIFTING CAPSULES 226 5.3.3 CONTROLLED FLIGHT AND THE ROLE OF THE
CENTER-OF-GRAVITY 230 5.3.4 SENSITIVITY OF AERODYNAMICS AGAINST SHAPE
VARIATIONS . 233 5.3.5 PARASITE TRIM 235 5.3.6 PERFORMANCE DATA OF
BICONES 237 5.3.7 INFLUENCE OF HIGH TEMPERATURE, REAL GAS EFFECTS ON
FORCES AND MOMENTS 241 5.4 DYNAMIC STABILITY 244 5.4.1 PHYSICS OF
DYNAMIC INSTABILITY 245 5.4.2 EQUATION OF ANGULAR MOTION 249 5.4.3
EXPERIMENTAL METHODS 253 5.4.4 NUMERICAL METHODS 257 5.4.5 TYPICAL
EXPERIMENTAL RESULTS 258 5.5 THERMAL LOADS 261 5.5.1 OREX SUBORBITAL
FLIGHT 262 5.5.2 ARD SUBORBITAL FLIGHT 263 5.5.3 APOLLO LOW EARTH ORBIT
(LEO) AND LUNAR RETURN . 265 5.5.4 VIKING-TYPE SHAPE TECHNOLOGY STUDY
267 5.6 PROBLEMS 273 REFERENCES 275 6 STABILIZATION, TRIM, AND CONTROL
DEVICES 279 6.1 CONTROL SURFACE AEROTHERMODYNAMICS, INTRODUCTION 279
6.1.1 FLAP EFFECTIVENESS: INFLUENCE OF THE ONSET FLOW FIELD. . 280 6.1.2
FLAP DEFLECTION MODES DURING HYPERSONIC FLIGHT 281 6.2 ONSET FLOW OF
AERODYNAMIC TRIM AND CONTROL SURFACES 282 6.2.1 OVERALL ONSET FLOW
CHARACTERISTICS 282 6.2.2 ENTROPY LAYER OF THE ONSET FLOW 287 6.2. TABLE
OF CONTENTS XIII 6.6.2 GEOMETRICAL CONSIDERATIONS 339 6.6.3 FLAP WIDTH
VERSUS FLAP LENGTH 340 6.6.4 VOLUMES OF STABILIZATION AND CONTROL
SURFACES 342 6.7 CONCLUDING REMARKS 347 6.7.1 SUMMARY OF RESULTS 347
6.7.2 SIMULATION ISSUES 349 6.8 PROBLEMS 351 REFERENCES 351 7 FORCES,
MOMENTS, CENTER-OF-PRESSURE, TRIM, AND STABILITY IN GENERAL FORMULATION
357 7.1 MOMENT EQUATION 357 7.2 GENERAL FORMULATION OF THE
CENTER-OF-PRESSURE 360 7.3 STATIC STABILITY CONSIDERATIONS FOR BLUFF
CONFIGURATIONS 363 7.4 STATIC STABILITY CONSIDERATIONS FOR SLENDER
CONFIGURATIONS.... 364 7.5 FURTHER CONTEMPLATIONS OF STATIC STABILITY
365 7.6 COORDINATE TRANSFORMATIONS OF FORCE COEFFICIENTS 367 7.7
PROBLEMS 369 REFERENCES 369 8 MULTIDISCIPLINARY DESIGN ASPECTS 371 8.1
INTRODUCTION AND SHORT OVERVIEW OF THE OBJECTIVES OF MULTIDISCIPLINARY
DESIGN WORK 373 8.2 EQUATIONS FOR FLUID-STRUCTURE INTERACTION DOMAINS
376 8.2.1 FLUID DYNAMICS EQUATIONS 376 8.2.2 STRUCTURE DYNAMICS
EQUATIONS 379 8.2.3 HEAT TRANSPORT EQUATION 381 8.3 COUPLING PROCEDURES
382 8.3.1 MECHANICAL FLUID-STRUCTURE INTERACTION AEROELASTIC APPROACH I
383 8.3.2 MECHANICAL FLUID-STRUCTURE INTERACTION AEROELASTIC APPROACH II
384 8.3.3 THERMAL-MECHANICAL FLUID-STRUCTURE INTERACTION 386 8.4
EXAMPLES OF COUPLED SOLUTIONS 389 8.4.1 MECHANICAL FLUID-STRUCTURE
INTERACTION AEROELASTI XIV TABLE OF CONTENTS 9 THE THERMAL STATE OF A
HYPERSONIC VEHICLE SURFACE 413 9.1 HEAT TRANSPORT AT A VEHICLE SURFACE
414 9.2 THE THERMAL STATE OF A VEHICLE SURFACE 416 9.3 AEROTHERMODYNAMIC
SIMULATION COMPENDIUM 418 9.3.1 GROUND-FACILITY SIMULATION 419 9.3.2
COMPUTATIONAL SIMULATION 420 9.3.3 IN-FLIGHT SIMULATION 422 REFERENCES
423 10 THE JEFF APPROACH AND APPROXIMATE RELATIONS 425 10.1 ELEMENTS OF
THE RHPM + FLYER: ^ E FF APPROACH AND BOW SHOCK TOTAL PRESSURE LOSS 425
10.1.1 INTRODUCTION AND DELINEATION 425 10.1.2 THE JEFF APPROACH:
GENERAL CONSIDERATIONS 426 10.1.3 NORMAL SHOCK WAVE 427 10.1.4 OBLIQUE
SHOCK WAVE 431 10.1.5 BOW SHOCK TOTAL PRESSURE LOSS: RESTITUTION OF
PARAMETERS OF A ONE-DIMENSIONAL SURFACE FLOW 433 10.1.6 THE
COMPRESSIBILITY FACTOR Z 434 10.1.7 RESULTS ACROSS SHOCKS IN THE LARGE
MI LIMIT USING JEFF 436 10.2 TRANSPORT PROPERTIES 437 10.3 FORMULAS FOR
STAGNATION POINT HEATING 439 10.4 FLAT SURFACE BOUNDARY LAYER PARAMETERS
BASED ON THE REFERENCE-TEMPERATURE/ENTHALPY CONCEPT 441 10.4.1
REFERENCE-TEMPERATURE/ENTHALPY CONCEPT 441 10.4. TABLE OF CONTENTS XV A.
2 EQUATIONS FOR EXCITATION OF MOLECULAR VIBRATIONS AND ELECTRON MODES
468 A.2.1 EXCITATION OF MOLECULAR VIBRATIONS 468 A.2.2 ELECTRON MODES
470 A.3 VECTOR FORM OF NAVIER-STOKES EQUATIONS INCLUDING THERMAL
NON-EQUILIBRIUM 471 REFERENCES 473 APPENDIX B. THE EARTH S ATMOSPHERE
475 REFERENCES 481 APPENDIX C. CONSTANTS, UNITS AND CONVERSIONS 483 C.I
CONSTANTS AND AIR PROPERTIES 483 C.2 UNITS AND CONVERSIONS 484
REFERENCES 486 APPENDIX D. SYMBOLS 487 D.I LATIN LETTERS 487 D.2 GREEK
LETTERS 492 D.3 INDICES 494 D.3.1 UPPER INDICES 494 D.3.2 LOWER INDICES
494 D.4 OTHER SYMBOLS 496 APPENDIX E. GLOSSARY, ABBREVIATIONS, ACRONYMS
499 E.I GLOSSARY 499 E.2 ABBREVIATIONS, ACRONYMS 501 PERMISSIONS 503
NAME INDEX 505 SUBJECT INDEX 511
|
| any_adam_object | 1 |
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| dewey-sort | 3629.133349 |
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| id | DE-604.BV035737766 |
| illustrated | Illustrated |
| indexdate | 2024-12-20T13:49:33Z |
| institution | BVB |
| isbn | 9783540899730 |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-018014232 |
| oclc_num | 458741398 |
| open_access_boolean | |
| owner | DE-83 DE-634 DE-91G DE-BY-TUM |
| owner_facet | DE-83 DE-634 DE-91G DE-BY-TUM |
| physical | XV, 518 S. Ill., graph. Darst. |
| publishDate | 2009 |
| publishDateSearch | 2009 |
| publishDateSort | 2009 |
| publisher | Springer |
| record_format | marc |
| spellingShingle | Hirschel, Ernst Heinrich 1934- Weiland, Claus Selected aerothermodynamic design problems of hypersonic flight vehicles Aerothermodynamik (DE-588)4133168-0 gnd Überschallflugzeug (DE-588)4186622-8 gnd Gestaltoptimierung (DE-588)4329076-0 gnd Hyperschallbereich (DE-588)4161092-1 gnd |
| subject_GND | (DE-588)4133168-0 (DE-588)4186622-8 (DE-588)4329076-0 (DE-588)4161092-1 |
| title | Selected aerothermodynamic design problems of hypersonic flight vehicles |
| title_auth | Selected aerothermodynamic design problems of hypersonic flight vehicles |
| title_exact_search | Selected aerothermodynamic design problems of hypersonic flight vehicles |
| title_full | Selected aerothermodynamic design problems of hypersonic flight vehicles Ernst Heinrich Hirschel ; Claus Weiland |
| title_fullStr | Selected aerothermodynamic design problems of hypersonic flight vehicles Ernst Heinrich Hirschel ; Claus Weiland |
| title_full_unstemmed | Selected aerothermodynamic design problems of hypersonic flight vehicles Ernst Heinrich Hirschel ; Claus Weiland |
| title_short | Selected aerothermodynamic design problems of hypersonic flight vehicles |
| title_sort | selected aerothermodynamic design problems of hypersonic flight vehicles |
| topic | Aerothermodynamik (DE-588)4133168-0 gnd Überschallflugzeug (DE-588)4186622-8 gnd Gestaltoptimierung (DE-588)4329076-0 gnd Hyperschallbereich (DE-588)4161092-1 gnd |
| topic_facet | Aerothermodynamik Überschallflugzeug Gestaltoptimierung Hyperschallbereich |
| url | http://deposit.dnb.de/cgi-bin/dokserv?id=3173859&prov=M&dok_var=1&dok_ext=htm http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=018014232&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
| work_keys_str_mv | AT hirschelernstheinrich selectedaerothermodynamicdesignproblemsofhypersonicflightvehicles AT weilandclaus selectedaerothermodynamicdesignproblemsofhypersonicflightvehicles |
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Teilbibliothek Maschinenwesen
| Signatur: |
0702 VER 516f 2011 A 2842 Lageplan |
|---|---|
| Exemplar 1 | Ausleihbar Am Standort |