Basic research and technologies for Two-Stage-to-Orbit vehicles: final report of the Collaborative Research Centres 253, 255 and 259
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| Language: | English |
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Weinheim
WILEY-VCH
2005
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| Online Access: | Inhaltsverzeichnis |
| Physical Description: | XVII, 666 S. Ill., graph. Darst. |
| ISBN: | 3527277358 9783527277353 |
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| 245 | 1 | 0 | |a Basic research and technologies for Two-Stage-to-Orbit vehicles |b final report of the Collaborative Research Centres 253, 255 and 259 |c Deutsche Forschungsgemeinschaft. Ed. by Dieter Jacob ... |
| 264 | 1 | |a Weinheim |b WILEY-VCH |c 2005 | |
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| adam_text | DEUTSCHE FORSCHUNGSGEMEINSCHAFT BASIC RESEARCH AND TECHNOLOGIES FOR
TWO-STAGE-TO-ORBIT VEHICLES FINAL REPORT OF THE COLLABORATIVE RESEARCH
CENTRES 253,255 AND 259 EDITED BY DIETER JACOB, GOTTFRIED SACHS AND
SIEGFRIED WAGNER WILEY- VCH WILEY-VCH VERLAG GMBH & CO. KGAA DFG
CONTENTS 1 INTRODUCTION 1 2 NETWORK ORGANIZATION OF COLLABORATIVE
RESEARCH CENTRES FOR SCIENTIFIC EFFICIENCY ENHANCEMENT 3 DIETER JACOB,
GOTTFRIED SACHS, AND SIEGFRIED WAGNER 2.1 INTRODUCTION 3 2.2
ORGANIZATION OF COLLABORATION 4 2.3 EFFICIENCY ENHANCEMENT IN RESEARCH 4
2.4 EFFICIENCY ENHANCEMENT IN TEACHING AND EDUCATION 5 2.5
INTERNATIONALIZATION 6 2.6 FINAL REMARKS **. 7 3 OVERALL DESIGN ASPECTS
: 9 3.1 CONCEPTUAL DESIGN OF WINGED REUSABLE TWO-STAGE-TO-ORBIT SPACE
TRANSPORT SYSTEMS 9 STEFAN LENTZ, MIRKO HORNUNG, AND WERNER STAUDACHER
3.1.1 BACKGROUND AND INTRODUCTION 9 3.1.2 CONCEPTS FOR REUSABLE SPACE
TRANSPORTS 11 3.1.2.1 SINGLE-STAGE-TO-ORBIT SSTO 11 3.1.2.2
TWO-STAGE-TO-ORBIT TSTO 12 3.1.3 DESIGN PROCEDURE 13 3.1.3.1 DESIGN
TOOLS AND METHODS 14 3.1.3.2 BASELINE CONCEPT 15 3.1.3.3 BOUNDARY
CONDITIONS AND REQUIREMENTS 16 BASIC RESEARCH AND TECHNOLOGIES TOR
TWO-STAGE-TO-ORBIT VEHICLES T DFG, DEUTSCHE FORSCHUNGSGEMEINSCHAFT
COPYRIGHT 2005 WILEY-VCH VERLAG GMBH & CO. KGAA, WEINHEIM ISBN:
3-527-27735-8 CONTENTS 3.1.3.4 VARIATION OF MISSION AND STAGING MACH
NUMBER 16 3.1.3.5 TRADE STUDIES 17 3.1.3.6 EVALUATION AND COMPARISON OF
THE CONCEPTS 17 3.1.4 VARIATION OF MISSION AND MACH NUMBERS 18 3.1.4.1
MISSION COMPARISON 20 3.1.4.2 COMPARISON OF MACH NUMBER VARIATION 21
3.1.4.3 ACCELERATOR VEHICLE CONCEPTS 25 3.1.5 TRADE STUDIES 25 3.1.5.1
AIRBREATHING SECOND STAGE 26 3.1.5.2 LOX-COLLECTION 29 3.1.6 COMPARISON
AND EVALUATION 34 3.1.7 CONCLUSION AND OUTLOOK 35 3.2 EVALUATION AND
MULTIDISCIPLINARY OPTIMIZATION OF TWO-STAGE-TO-ORBIT SPACE PLANES WITH
DIFFERENT LOWER-STAGE CONCEPTS 38 THORSTEN RAIBLE AND DIETER JACOB 3.2.1
INTRODUCTION 38 3.2.2 REFERENCE CONFIGURATIONS 40 3.2.2.1 CONCEPT DESIGN
AND MISSION REQUIREMENTS 40 3.2.2.2 SPACE PLANE CONFIGURATION WITH
LIFTING BODY LOWER STAGE 40 3.2.2.3 SPACE PLANE CONFIGURATION WITH
WAVERIDER LOWER STAGE 42 3.2.2.4 DESIGN AND OPTIMIZATION PARAMETERS 44
3.2.3 ANALYSIS METHODS 44 3.2.3.1 QUALITY CRITERIA 44 3.2.3.2 SIMULATION
AND OPTIMIZATION SOFTWARE 46 3.2.4 PERFORMANCEFQF REFERENCE SPACE PLANES
46 3.2.4.1 MASS BREAKDOWN 46 3.2.4.2 DESIGN SENSITIVITIES 48 3.2.5
OPTIMIZATION RESULTS 50 3.2.5.1 NOMINAL OPTIMIZATIONS 50 3.2.5.2
SENSITIVITY-BASED OPTIMIZATIONS 53 3.2.6 SUMMARY AND CONCLUSIONS 54 4
AERODYNAMICS AND THERMODYNAMICS 57 4.1 LOW-SPEED TESTS WITH AN
ELAC-MODEL AT HIGH REYNOLDS NUMBERS 57 GTINTHER NEUWERTH, UDO PEITER,
AND DIETER JACOB 4.1.1 INTRODUCTION 58 4.1.2 WIND TUNNEL MODELS 59 4.1.3
PRESSURE DISTRIBUTIONS INFLUENCED BY REYNOLDS NUMBER 61 4.1.4 FLOW FIELD
INFLUENCED BY REYNOLDS NUMBER 67 4.1.5 FORCE COEFFICIENTS INFLUENCED BY
REYNOLDS NUMBER 71 4.1.6 CONCLUSION 75 VI CONTENTS 4.2 EXPERIMENTAL AND
NUMERICAL ANALYSIS OF SUPERSONIC FLOW OVER THE ELAC-CONFIGURATION 77
ANATOLY MICHAILOVICH KHARITONOV, MARK DAVIDOVICH BRODETSKY, ANDREAS
HENZE, WOLFGANG SCHRODER, MATTHIAS HELLER, GOTTFRIED SACHS, CHRISTIAN
BREITSAMTER, AND BORIS LASCHKA 4.2.1 INTRODUCTION 77 4.2.2 EXPERIMENTAL
SETUP 78 4.2.3 NUMERICAL METHOD 87 4.2.4 RESULTS 88 4.2.4.1 FLOW OVER
THE ORBITAL STAGE AND THE EOS/FLAT PLATE CONFIGURATION 88 4.2.4.2
SEPARATION OF ELAC1C AND EOS 96 4.2.5 CONCLUSIONS 100 4.3 STAGE
SEPARATION - AERODYNAMICS AND FLOW PHYSICS 101 CHRISTIAN BREITSAMTER,
LEI JIANG, AND MOCHAMMAD AGOES MOELYADI 4.3.1 INTRODUCTION 102 4.3.2
METHODOLOGY AND VEHICLE GEOMETRIES 102 4.3.3 NUMERICAL SIMULATION 105
4.3.3.1 FLOW SOLVER 105 4.3.3.2 GRID GENERATION 106 4.3.4 EXPERIMENTAL
SIMULATION 107 4.3.4.1 MODELS AND FACILITY 107 4.3.4.2 MEASUREMENT
TECHNIQUE AND TEST PROGRAMME 108 4.3.5 STEADY STATE FLOW 109 4.3.5.1
DOMINANT FLOW PHENOMENA 109 4.3.5.1.1 INVISCID CASE - 2D AND 3D
SIMULATIONS 109 4.3.5.1.2 VISCOUS EFFECTS - LAMINAR AND TURBULENT FLOW
112 4.3.5.2 COMPARISON OF EXPERIMENTAL AND NUMERICAL RESULTS 113 4.3.6
UNSTEADY AERODYNAMICS .115 4.3.6.1 LONGITUDINAL MOTION - DYNAMIC
SEPARATION 115 4.3.6.2 LATERAL MOTION - DISTURBANCE EFFECTS 117 4.3.7
DETAILED TWO-STAGE-TO-ORBIT CONFIGURATION 119 4.3.8 CONCLUSIONS AND
OUTLOOK 122 4.4 DNS OF LAMINAR-TURBULENT TRANSITION IN THE LOW
HYPERSONIC REGIME 124 AXEL FEZER, MARKUS KLOKER, ALESSANDRO PAGELLA,
ULRICH RIST, AND SIEGFRIED WAGNER 4.4.1 INTRODUCTION 124 4.4.2 NUMERICAL
APPROACH 125 4.4.2.1 GOVERNING EQUATIONS 126 4.4.2.2 SPATIAL AND TIME
DISCRETIZATION 127 4.4.2.3 INITIAL AND BOUNDARY CONDITIONS 127 4.4.3
TRANSITION ON FLAT PLATE AND SHARP CONE 128 VII CONTENTS 4.4.3.1
APPLICATION-SPECIFIC DETAILS OF THE NUMERICAL METHOD 128 4.4.3.2
RESULTS: SIMULATION OF A CONTROLLED EXPERIMENT 130 4.4.3.3 RESULTS: FLAT
PLATE AND CONE AT M = 6.8 131 4.4.4 TRANSITIONAL
SHOCK-WAVE/BOUNDARY-LAYER INTERACTION AT MA = 4.8 135 4.4.4.1
APPLICATION-SPECIFIC DETAILS OF THE NUMERICAL METHOD 137 4.4.4.2
RESULTS: IMPINGING SHOCK ON A FLAT PLATE VS. COMPRESSION RAMP AT MA =
4.8 139 4.4.4.3 CONCLUSIONS 146 4.5 NUMERICAL SIMULATION OF
HIGH-ENTHALPY NONEQUILIBRIUM AIR FLOWS 148 FARID INFED, MARKUS FERTIG,
FERDINAND OLAWSKY, PANAGIOTIS ADAMIDIS, MONIKA AUWETER-KURTZ, MICHAEL
RESCH, AND ERNST W. MESSERSCHMID 4.5.1 AEROTHERMODYNAMIC ASPECTS OF
RE-ENTRY FLOWS 148 4.5.1.1 INVISCID FLUXES 149 4.5.1.2 THERMAL
RELAXATION 150 4.5.1.3 ELECTRONIC EXCITATION 150 4.5.1.4 THERMOCHEMICAL
RELAXATION 151 4.5.1.5 TRANSPORT COEFFICIENTS 152 4.5.1.6 TURBULENCE 152
4.5.1.7 ELECTRICAL DISCHARGE 152 4.5.1.8 GAS-SURFA EE INTERACTION
MODELLING 152 4.5.1.9 RADIATIVE EXCHANGE AT THE SURFACE 153 4.5.1.10
HEAT CONDUCTION WITHIN TPS MATERIALS 154 4.5.2 NUMERICS AND
PARALLELIZATION 155 4.5.2.1 CONSERVATION EQUATIONS 155 4.5.2.2 SOLVER
156 4.5.2.3 MULTIBLOCK 157 4.5.2.4 METACOMPUTING . 158 4.5.2.5 ADAPTIVE
GRIDS 1 58 4.5.3 RESULTS 159 4.5.3.1 SIMULATION OF THE RE-ENTRY OF THE
X-38 159 4.5.3.2 SIMULATION OF THE PLASMA SOURCE RD5 162 4.6 FLOW
SIMULATION AND PROBLEMS IN GROUND TEST FACILITIES 165 I/WE GAISBAUER,
HELMUT KNAUSS, SIEGFRIED WAGNER, GEORG HERDRICH, MARKUS FERTIG, MICHAEL
WINTER, AND MONIKA AUWETER-KURTZ 4.6.1 INTRODUCTION 165 4.6.2 VALIDATION
OF A SHORT DURATION SUPERSONIC WIND TUNNEL FOR NATURAL LAMINAR TURBULENT
TRANSITION STUDIES 170 4.6.2.1 INTRODUCTION TO THE PROBLEM 170 4.6.2.2
THE SHOCK WIND TUNNEL AT STUTTGART UNIVERSITY 171 4.6.2.3 DETECTION
TECHNIQUES FOR FLOW DISTURBANCE FIELDS 175 VIII CONTENTS 4.6.2.4 FREE
STREAM DISTURBANCE MEASUREMENTS IN THE SHOCK WIND TUNNEL 178 4.6.2.5
TRANSITION EXPERIMENTS IN THE TEST SECTION FLOW 184 4.6.2.6 CONCLUSION
AND ASPECTS 189 4.6.3 PLASMA WIND TUNNELS 191 4.6.3.1 PLASMA GENERATORS
192 4.6.3.1.1 ARC-DRIVEN PLASMA GENERATORS (TPG AND MPG) 192 4.6.3.1.2
INDUCTIVELY HEATED PLASMA GENERATORS (IPGS) 195 4.6.3.2 HEAT FLUX
SIMULATION FOR X-38 USING PWK1 AS EXAMPLE FOR PWK INVESTIGATION 197 4.7
CHARACTERIZATION OF HIGH-ENTHALPY FLOWS 199 MONIKA AUWETER-KURTZ, MARKUS
FERTIG, GEORG HERDRICH, KURT HIRSCH, STEFAN LOHLE, SERGEJ PIDAN, UWE
SCHUMACHER, AND MICHAEL WINTER 4.7.1 INTRUSIVE MEASUREMENT METHODS 200
4.7.1.1 MATERIAL SAMPLE SUPPORT SYSTEM 202 4.7.1.2 HEAT FLUX
MEASUREMENTS 203 4.7.2 NON-INTRUSIVE TECHNIQUES 206 4.7.2.1 EMISSION
SPECTROSCOPY 207 4.7.2.2 LASER-INDUCED FLUORESCENCE 209 4.7.2.3 THOMSON
SCATTERING FOR ELECTRON TEMPERATURE AND DENSITY DETERMINATION 211
4.7.2.4 HIGH-RESOLUTION SPECTROSCOPY AND FABRY PEROT INTERFEROMETRY . .
212 4.7.3 FLIGHT INSTRUMENTATION (PYREX, RESPECT, PHLUX, COMPARE) . 213
4.7.3.1 DESCRIPTION OF PYREX-KAT38 (PYROMETRIC ENTRY EXPERIMENT) ... 214
4.7.3.2 RESPECT (RE-ENTRY SPECTROMETER) 216 4.7.3.3 COMPARE 217 4.8
NUMERICAL SIMULATION OF FLOW FIELDS PAST SPACE TRANSPORTATION SYSTEMS
220 ANDREAS HENZE, WOLFGANG SCHRODER, AND MATTHIAS MEINKE 4.8.1
INTRODUCTION 221 4.8.2 NUMERICAL SCHEME 221 4.8.2.1 BASIC EQUATIONS 221
4.8.2.2 INITIAL AND BOUNDARY CONDITIONS 222 4.8.2.3 SPATIAL
DISCRETIZATION IN STRUCTURED GRIDS 223 4.8.2.4 SPATIAL DISCRETIZATION IN
UNSTRUCTURED GRIDS 224 4.8.2.5 STRUCTURED/UNSTRUCTURED COUPLING 225
4.8.2.6 TEMPORAL INTEGRATION 225 4.8.3 RESULTS 226 4.8.3.1 GEOMETRY OF
THE TWO-STAGE SYSTEM 226 4.8.3.2 FLOW PAST ELAC 228 4.8.3.3 FLOW PAST
ELAC-LC 233 4.8.3.4 SIMPLIFIED STAGE SEPARATION 240 4.8.4 CONCLUSIONS
241 IX CONTENTS 4.9 HIGH-SPEED AERODYNAMICS OF THE TWO-STAGE ELAC/EOS-
CONFIGURATION FOR ASCEND AND RE-ENTRY 242 MARTIN BLEILEBENS, CHRISTOPH
GLOBNER, AND HERBERT OLIVIER 4.9.1 INTRODUCTION AND EXPERIMENTAL
CONDITIONS 242 4.9.2 MEASUREMENT EQUIPMENT 244 4.9.2.1 PRESSURE
MEASUREMENT 244 4.9.2.2 TEMPERATURE AND HEATFLUX MEASUREMENT 244 4.9.2.3
FORCE AND MOMENT MEASUREMENT 244 4.9.2.4 FLOW VISUALIZATION 245 4.9.3
MEASUREMENTS ON THE ELAC- AND EOS-CONFIGURATIONS 246 4.9.3.1 PRESSURE
AND HEAT FLUX MEASUREMENTS ON THE ELAC-CONFIGURATION 246 4.9.3.2 FORCE
AND MOMENT MEASUREMENTS ON THE ELAC-CONFIGURATION . . 247 4.9.3.3
PRESSURE AND HEAT FLUX MEASUREMENTS ON THE EOS- CONFIGURATION 249
4.9.3.4 FORCE AND MOMENT MEASUREMENTS ON THE EOS-CONFIGURATION . . . 251
4.9.4 DETAILED MEASUREMENTS ON RAMP-CONFIGURATIONS 254 4.9.4.1 LAMINAR
AND TURBULENT SHOCK-WAVE/BOUNDARY-LAYER INTERACTIONS 254 4.9.4.2
THEORETICAL CONSIDERATIONS 255 4.9.4.3 RAMP FLOWS WITH VARIATION OF
SURFACE TEMPERATURE 256 4.9.4.4 DESCRIPTION OF RAMP MODEL 258 4.9.4.5
SCHLIEREN PICTURES AND POSITION OF SEPARATION 260 4.9.4.6 DETERMINATION
OF PRESSURE COEFFICIENTS 262 4.9.4.7 DETERMINATION OF STANTON NUMBERS
264 4.9.5 CONCLUSIONS 267 5 PROPULSION 269 5.1 PDF/FDF-METHODS FOR THE
PREDICTION OF SUPERSONIC TURBULENT COMBUSTION 269 STEFAN HEINZ AND
RAINER FRIEDRICH 5.1.1 INTRODUCTION 269 5.1.2 METHODS FOR TURBULENT
REACTING FLOW CALCULATIONS 270 5.1.2.1 BASIC METHODS 271 5.1.2.2 HYBRID
PDF/FDF-METHODS 272 5.1.3 SOME DEFICIENCIES OF EXISTING HYBRID
PDF-METHODS 272 5.1.3.1 THE TRANSPORT PROBLEM 273 5.1.3.2 THE MIXING
PROBLEM 273 5.1.3.3 THE ENERGY PROBLEM 274 5.1.4 NEW THEORETICAL
CONCEPTS 275 5.1.4.1 THE TRANSPORT PROBLEM 276 5.1.4.2 THE MIXING
PROBLEM 276 5.1.4.3 THE ENERGY PROBLEM 276 5.1.5 THE USE OF PDF
COMBUSTION CODES 277 5.1.5.1 THE CURRENT USE OF PDF/FDF-METHODS 277 X
CONTENTS 5.1.5.2 NEW DEVELOPMENTS 279 5.1.5.3 COMMON ACTIVITIES TO
DEVELOP A NEW COMBUSTION CODE 279 5.1.6 PROSPECTS FOR FURTHER
DEVELOPMENTS 280 5.1.6.1 THE CURRENT AND FUTURE USE OF COMPUTATIONAL
METHODS 280 5.1.6.2 SOME CHALLENGES 281 5.2 DESIGN AND TESTING OF
GASDYNAMICALLY OPTIMIZED FUEL INJECTORS FOR THE PILOTING OF SUPERSONIC
FLAMES WITH LOW LOSSES 284 ANATOLIY LYUBAR, TOBIAS SANDER, AND THOMAS
SATTELMAYER 5.2.1 INTRODUCTION 284 5.2.2 EXPERIMENTAL SETUP 285 5.2.2.1
MODEL SCRAMJET COMBUSTOR 285 5.2.2.2 PREHEATER 285 5.2.2.3 COMBUSTION
CHAMBER 286 5.2.2.4 INJECTORS 288 5.2.3 INVESTIGATION TOOLS 289 5.2.3.1
SHADOWGRAPH METHOD 289 5.2.3.2 RAYLEIGH SCATTERING 289 5.2.3.3 RAMAN
SCATTERING 289 5.2.3.4 OH-LIF MEASUREMENTS 290 5.2.3.5 SELF-FLUORESCENCE
MEASUREMENTS (CHEMILUMINESCENCE) 290 5.2.4 NUMERICAL MODELLING 291
5.2.4.1 NUMERICAL SIMULATION WITH THE CFD-CODE FLUENT 5.5 291 5.2.4.2
SPECIAL FEATURES OF THE MODELLING OF THE SUPERSONIC COMBUSTION 291
5.2.4.3 REDUCING THE NUMBER OF SPECIES 292 5.2.4.4 REACTION MAPPING BY
USING OF THE POLYNOMIALS 294 5.2.4.5 VALIDATION OF THE MODELLING
APPROACH WITH POLYNOMIALS 295 5.2.5 TWO STAGE INJECTOR 297 5.2.5.1
THEORETICAL CONSIDERATIONS 297 5.2.5.2 SHOCK STABILIZATION 300 5.2.5.3
COMBUSTION *.. 303 5.2.6 CONCLUSIONS 305 5.3 HYPERSONIC PROPULSION
SYSTEMS: DESIGN, DUAL-MODE COMBUSTION AND SYSTEMS OFF-DESIGN SIMULATION
308 5.3.1 COMBUSTION STABILITY OF A DUAL-MODE SCRAMJET - CONFIGURATION
WITH STRUT INJECTOR 308 SARA ROCCI-DENIS, ARMIN BRANDSTETTER, DIETER
RIST, AND HANS-PETER KAU 5.3.1.1 INTRODUCTION 308 5.3.1.2 EXPERIMENTAL
SETUP 310 5.3.1.3 RESULTS AND DISCUSSION 315 5.3.1.4 CONCLUSIONS 324 XI
CONTENTS 5.3.2 HYPERSONIC HIGHLY INTEGRATED PROPULSION SYSTEMS - DESIGN
AND OFF-DESIGN SIMULATION 327 HANS RICK, ANDREAS BAUER, THOMAS ESCH,
SEBASTIAN HOLLMEIER, HANS-PETER KAU, SVEN KOPP, AND ANDREAS KREINER
5.3.2.1 INTRODUCTION 327 5.3.2.2 REFERENCE PROPULSION SYSTEM FOR THE
TSTO CONCEPT 330 5.3.2.3 ENGINE INTEGRATION 330 5.3.2.4 CORE ENGINE .
336 5.3.2.5 NUMERICAL ENGINE SIMULATION 337 5.3.2.6 THRUST VECTORING 338
5.3.2.7 REAL TIME FLIGHT SIMULATION 344 5.3.2.8 CONCLUSION 345 5.4
EXPERIMENTAL INVESTIGATION ABOUT EXTERNAL COMPRESSION OF HIGHLY
INTEGRATED AIRBREATHING PROPULSION SYSTEMS 347 I/WE GAISBAUER, HELMUT
KNAUSS, AND SIEGFRIED WAGNER 5.4.1 INTRODUCTION 347 5.4.1.1 FOCUS ON THE
PROBLEM 348 5.4.1.2 PRELIMINARY MEASUREMENTS 349 5.4.2 EXPERIMENTAL
FACILITY 350 5.4.3 WIND TUNNEL MODELS AND INSTRUMENTATION 351 5.4.3.1
MODEL 1 351 5.4.3.2 MODEL 2 352 5.4.3.3 MODEL 3 353 5.4.4 NUMERICAL
MODEL 354 5.4.5 MEASUREMENTS AND RESULTS 354 5.4.5.1 DETERMINATION OF
THE BOUNDARY-CONDITIONS 355 5.4.5.2 MEASUREMENTS IN THE FIELD OF SHOCK
BOUNDARY LAYER INTERACTION 358 5.4.6 CONCLUSION AND OUTLOOK 362 5.5
EXPERIMENTAL AND NUMERICAL INVESTIGATION OF LOBED STRUT INJECTORS FOR
SUPERSONIC COMBUSTION 365 PETER GERLINGER, PETER KASAL, FERNANDO
SCHNEIDER, JENS VON WOLFERSDORF, BERNHARD WEIGANG, AND MANFRED AIGNER
5.5.1 INTRODUCTION 365 5.5.2 EXPERIMENTAL SETUP AND MEASUREMENT
TECHNIQUES 366 5.5.3 GOVERNING EQUATIONS AND NUMERICAL SIMULATION 369
5.5.3.1 MULTIGRID CONVERGENCE ACCELERATION 370 5.5.4 STRUT DESIGN AND
PERFORMANCE PARAMETERS 371 5.5.5 SUPERSONIC MIXING 373 5.5.6 SUPERSONIC
COMBUSTION 374 5.5.6.1 INVESTIGATION OF DIFFERENT LOBED STRUT INJECTORS
375 5.5.7 CONCLUSIONS 380 XII CONTENTS 5.6 EXPERIMENTAL STUDIES OF
VISCOUS INTERACTION EFFECTS IN HYPERSONIC INLETS AND NOZZLE FLOW FIELDS
383 ANDREAS HENCKELS AND PATRICK GRUHN 5.6.1 INTRODUCTION 383 5.6.2
EXPERIMENTAL TECHNIQUES 385 5.6.2.1 FACILITY AND FLOW DIAGNOSTICS 385
5.6.2.2 WIND TUNNEL MODELS 386 5.6.3 INLET STUDIES 388 5.6.4 NOZZLE
STUDIES 395 5.6.5 CONCLUSION 400 5.7 INTAKE FLOWS IN AIRBREATHING
ENGINES FOR SUPERSONIC AND HYPERSONIC TRANSPORT 403 BIRGIT URSULA
REINARTZ, JOERN VAN KEUK, JOSEF BALLMANN, CARSTEN HERRMANN, AND WOLFGANG
KOSCHEL 5.7.1 INTRODUCTION 404 5.7.2 PHYSICAL MODEL 405,, 5.7.3
NUMERICAL METHOD 406 * 5.7.4 RESULTS 408 5.7A.I TURBULENT 2D SUPERSONIC
INTAKE FLOWS WITH INTERNAL COMPRESSION 408 5.7.4.2 LAMINAR 3D HYPERSONIC
CORNER FLOWS 411 5.7.4.3 TURBULENT 3D HYPERSONIC FLOWS THROUGH
SYMMETRIC/ASYMMETRIC DOUBLE-FIN CONFIGURATIONS 414 5.7.4.4 LAMINAR 2D
SHOCK INTERACTIONS IN HYPERSONIC FLOWS WITH CHEMICAL NON-EQUILIBRIUM 415
5.7.5 CONCLUSIONS 418 6 FLIGHT MECHANICS AND CONTROL 421 6.1 SAFETY
IMPROVEMENT FOR TWO-STAGE-TO-ORBIT VEHICLES BY APPROPRIATE MISSION ABORT
STRATEGIES 421 MICHAEL MAYRHOFER, OTTO WAGNER, AND GOTTFRIED SACHS 6.1.1
INTRODUCTION 422 6.1.2 DYNAMICS MODEL OF TWO-STAGE-TO-ORBIT VEHICLE 423
6.1.3 OPTIMIZATION PROBLEM 427 6.1.4 SAFETY IMPROVED NOMINAL TRAJECTORY
428 6.1.5 MISSION ABORTS OF CARRIER STAGE 430 6.1.6 MISSION ABORTS OF
ORBITAL STAGE 432 6.1.7 MISSION ABORT PLAN 435 6.1.8 CONCLUSIONS 436
XIII CONTENTS 6.2 OPTIMAL TRAJECTORIES FOR HYPERSONIC VEHICLES WITH
PREDEFINED LEVELS OF INHERENT SAFETY 438 RAINER CALLIES 6.2.1
INTRODUCTION 439 6.2.2 THEORETICAL BACKGROUND 440 6.2.2.1 CLASSICAL
PROBLEM 440 6.2.2.2 RELATED BOUNDARY VALUE PROBLEM 440 6.2.2.3 EXTENDED
PROBLEM (A) 441 6.2.2.4 EXTENDED PROBLEM (B) 444 6.2.3 NUMERICAL METHOD
446 6.2.4 MODEL SYSTEM 449 6.2.4.1 OVERVIEW 449 6.2.4.2 THRUST MODEL 449
6.2.4.3 ATMOSPHERIC AND AERODYNAMIC MODEL 450 6.2.4.4 EQUATIONS OF
MOTION 451 6.2.4.5 PRIMARY PROBLEM 452 6.2.4.6 SECONDARY PROBLEM 453
6.2.4.7 EXTENDED PROBLEM (B) 454 6.2.4.8 NUMERICAL RESULTS 455 6.2.5
CONCLUSION 456 6.3 HYPERSONIC TRAJECTORY OPTIMIZATION FOR THERMAL LOAD
REDUCTION 458 MICHAEL DINKELMANN, MARKUS WACHTER, AND GOTTFRIED SACHS
6.3.1 INTRODUCTION 459 6.3.2 MODELLING OF VEHICLE DYNAMICS 460 6.3.3
MODELLING OF HEAT INPUT 464 6.3.4 OPTIMIZATION PROBLEM 467 6.3.5 RESULTS
469 6.3.5.1 RANGE CRUISE 469 6.3.5.2 RETURN-TO-BASE CRUISE 471 6.3.6
CONCLUSIONS 473 6.4 FLIGHT DYNAMICS AND CONTROL PROBLEMS OF
TWO-STAGE-TO-ORBIT VEHICLES 476 6.4.1 FLIGHT TESTS AND SIMULATION
EXPERIMENTS FOR HYPERSONIC LONG-TERM DYNAMICS FLYING QUAHTIES 476 ROBERT
STICH, TIMOTHY H. COX, AND GOTTFRIED SACHS 6.4.1.1 INTRODUCTION 477
6.4.1.2 HYPERSONIC FLIGHT DYNAMICS 478 6.4.1.3 RESEARCH AIRCRAFT AND
FLIGHT SIMULATOR 480 6.4.1.4 RESULTS 482 6.4.1.5 CONCLUSIONS 487 XIV
CONTENTS 6.4.2 WIND TUNNEL TESTS FOR MODELLING THE SEPARATION DYNAMICS
OF A TWO-STAGE-TO-ORBIT VEHICLE 489 CHRISTIAN ZDHRINGER AND GOTTFRIED
SACHS 6.4.2.1 INTRODUCTION 489 6.4.2.2 TEST FACILITY AND WIND TUNNEL
MODELS 490 6.4.2.3 RESULTS 492 6.4.2.4 CONCLUSIONS 497 7
HIGH-TEMPERATURE MATERIALS AND HOT STRUCTURES 499 7.1 CERAMIC MATRIX
COMPOSITES - THE KEY MATERIALS FOR RE-ENTRY FROM SPACE TO EARTH 499
MARTIN FRIEB, WALTER KRENKEL, RICHARD KOCHENDORFER, RIIDIGER BRANDT,
GIINTHER NEUER, AND HANS-PETER MAIER 7.1.1 INTRODUCTION AND OVERVIEW 499
7.1.2 LIQUID SILICON INFILTRATION: PROCESS DEVELOPMENT 500 7.1.3
MICROSTRUCTURAL DESIGN OF C/C-SIC COMPOSITES 502 7.1.3.1 C/C-SIC
COMPOSITES DERIVED FROM AS-RECEIVED CARBON FIBRES . . 502 7.1.3.2
C/C-SIC COMPOSITES DERIVED FROM THERMALLY PRE-TREATED CARBON FIBRES 503
7.1.3.3 GRADED C/C-SIC COMPOSITES 504 7.1.3.4 C/C-SIC COMPOSITES DERIVED
FROM GRAPHITIZED C/C 508 7.1.4 MACROSCOPIC DESIGN ASPECTS 509 7.1.4.1
DIMENSIONAL STABILITY 509 7.1.4.2 MODULAR CONSTRUCTION BY IN-SITU
JOINING 511 7.1.5 THERMOPHYSICAL CHARACTERIZATION OF C/C-SIC 512 7.1.5.1
METHODS TO MEASURE THERMOPHYSICAL PROPERTIES 512 7.1.5.2 MATERIALS AND
SPECIMEN PREPARATION 512 7.1.5.3 SPECIFIC HEAT CAPACITY . 514 7.1.5.4
THERMAL CONDUCTIVITY . 515 7.1.5.5 SPECTRAL AND TOTAL EMISSIVITY 518
7.1.6 THERMOMECHANICAL CHARACTERIZATION OF C/C-SIC 520 7.1.6.1 FAILURE
MECHANISM OF C/C-SIC MATERIALS 520 7.1.6.2 INFLUENCE OF THE TEMPERATURE
ON THE STRESS-STRAIN BEHAVIOUR .... 520 7.2 BEHAVIOUR OF REUSABLE HEAT
SHIELD MATERIALS UNDER RE-ENTRY CONDITIONS 527 FRITZ ALDINGER, MONIKA
AUWETER-KURTZ, MARKUS FERTIG, GEORG HERDRICH, KURT HIRSCH, PETER
LINDNER, DIRK MATUSCH, GIINTHER NEUER, UWE SCHUMACHER, AND MICHAEL
WINTER 7.2.1 PRINCIPLES AND MODELLING OF HETEROGENEOUS REACTIONS 528
7.2.1.1 HETEROGENEOUS CATALYSIS 528 7.2.1.2 REDOX REACTIONS INCLUDING
ACTIVE AND PASSIVE OXIDATION 531 7.2.1.3 SURFACE REACTION MODEL APPLIED
TO MIRKA RE-ENTRY FLOW 533 XV CONTENTS 7.2.2 CHARACTERIZATION OF
HIGH-TEMPERATURE OXIDATION AND CATALYTIC BEHAVIOUR OF TPS MATERIALS 535
7.2.2.1 EXPERIMENTALLY OBSERVED INFLUENCE OF CATALYTIC EFFICIENCY 535
7.2.2.2 OXIDATION BEHAVIOUR 537 7.2.3 DEVELOPMENTS AND INVESTIGATIONS OF
PROTECTION LAYERS FOR REUSABLE HEAT SHIELD MATERIALS 541 7.2.3.1
PRODUCTION AND CHARACTERISTICS OF PROTECTION LAYERS 541 7.2.3.2
DIAGNOSTICS FOR THE TESTS OF THE PROTECTION LAYERS IN THE PLASMA WIND
TUNNEL 542 7.2.3.3 PROTECTION MATERIAL TESTS AND RESULTS 543 7.3 DESIGN
AND EVALUATION OF FIBRE CERAMIC STRUCTURES 549 BERND-HELMUT KROPLIN,
RICHARD KOCHENDORFER, THOMAS REIMER, THOMAS ULLMANN, RALF KORNMANN,
ROGER SCHAFER, AND THOMAS WALLMERSPERGER 7.3.1 INTRODUCTION 549 7.3.1.1
CONCEPT DESIGN AND MANUFACTURING STUDIES 551 7.3.1.2 MANUFACTURING 553
7.3.1.3 TEST 554 7.3.1.4 PLASMA SPRAYED YTTRIUM SILICATES FOR OXIDATION
PROTECTION OF C/C-SIC PANELS 555 7.3.1.5 FLIGHT EXPERIMENT 557 7.3.2
MEASURING MODEL DEFLECTIONS BY THERMO-MECHANICAL LOADS IN A PLASMA WIND
TUNNEL 559 7.3.2.1 OVERVIEW 559 7.3.2.2 MODEL DESIGN 561 7.3.2.3
ADAPTATION OF THE HTGM TO THE L3K FACILITY 562 7.3.2.4 RESULTS 565 7.3.3
MATERIAL DESCRIPTION OF FIBRE CERAMICS 569 7.3.3.1 PHENOMENA IN C/C-SIC
MATERIALS 569 7.3.3.2 PHENOMENOLOGICAL MODEL 571 7.3.3.3
MICROMECHANICALLY BASED PHENOMENOLOGICAL MODEL 573 7.3.3.4 FUNCTIONALLY
GRADED MATERIALS 575 7.3.4 CONCLUSIONS 578 COOPERATION WITH INDUSTRY AND
RESEARCH ESTABLISHMENTS, PARTICIPATION IN NATIONAL AND INTERNATIONAL
RESEARCH PROGRAMMES 581 DIETER JACOB, GOTTFRIED SACHS, AND SIEGFRIED
WAGNER CONCLUSIONS AND PERSPECTIVES 585 DIETER JACOB, GOTTFRIED SACHS,
AND SIEGFRIED WAGNER XVI CONTENTS 10 APPENDIX 587 10.1 PUBLICATIONS 587
10.2 DISSERTATIONS 639 10.3 HABILITATIONS 648 10.4 PATENTS 649 10.5
NUMBER OF DIPLOMA THESES 649 10.6 VISITING RESEARCHERS 649 10.7
ORGANIZATION AND PROJECTS 656 XVII
|
| any_adam_object | 1 |
| building | Verbundindex |
| bvnumber | BV019815472 |
| callnumber-first | T - Technology |
| callnumber-label | TL1050 |
| callnumber-raw | TL1050 |
| callnumber-search | TL1050 |
| callnumber-sort | TL 41050 |
| callnumber-subject | TL - Motor Vehicles and Aeronautics |
| classification_rvk | US 9500 ZO 8300 |
| classification_tum | VER 820f |
| ctrlnum | (OCoLC)72889566 (DE-599)BVBBV019815472 |
| dewey-full | 629.4 |
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| dewey-ones | 629 - Other branches of engineering |
| dewey-raw | 629.4 |
| dewey-search | 629.4 |
| dewey-sort | 3629.4 |
| dewey-tens | 620 - Engineering and allied operations |
| discipline | Maschinenbau / Maschinenwesen Physik Verkehrstechnik Verkehr / Transport |
| format | Book |
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| id | DE-604.BV019815472 |
| illustrated | Illustrated |
| indexdate | 2024-07-09T20:06:46Z |
| institution | BVB |
| institution_GND | (DE-588)5037500-3 |
| isbn | 3527277358 9783527277353 |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-013140818 |
| oclc_num | 72889566 |
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| physical | XVII, 666 S. Ill., graph. Darst. |
| publishDate | 2005 |
| publishDateSearch | 2005 |
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| publisher | WILEY-VCH |
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| spelling | Basic research and technologies for Two-Stage-to-Orbit vehicles final report of the Collaborative Research Centres 253, 255 and 259 Deutsche Forschungsgemeinschaft. Ed. by Dieter Jacob ... Weinheim WILEY-VCH 2005 XVII, 666 S. Ill., graph. Darst. txt rdacontent n rdamedia nc rdacarrier Space vehicles Aerodynamics Raumtransporter (DE-588)4177083-3 gnd rswk-swf Technologie (DE-588)4059276-5 gnd rswk-swf Raumfahrttechnik (DE-588)4177061-4 gnd rswk-swf Raumfahrzeug (DE-588)4048579-1 gnd rswk-swf (DE-588)4143413-4 Aufsatzsammlung gnd-content Raumfahrzeug (DE-588)4048579-1 s Technologie (DE-588)4059276-5 s DE-604 Raumtransporter (DE-588)4177083-3 s Raumfahrttechnik (DE-588)4177061-4 s DE-188 Jacob, Dieter Sonstige oth Sonderforschungsbereich Grundlagen des Entwurfs von Raumflugzeugen Sonstige (DE-588)5037500-3 oth GBV Datenaustausch application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=013140818&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
| spellingShingle | Basic research and technologies for Two-Stage-to-Orbit vehicles final report of the Collaborative Research Centres 253, 255 and 259 Space vehicles Aerodynamics Raumtransporter (DE-588)4177083-3 gnd Technologie (DE-588)4059276-5 gnd Raumfahrttechnik (DE-588)4177061-4 gnd Raumfahrzeug (DE-588)4048579-1 gnd |
| subject_GND | (DE-588)4177083-3 (DE-588)4059276-5 (DE-588)4177061-4 (DE-588)4048579-1 (DE-588)4143413-4 |
| title | Basic research and technologies for Two-Stage-to-Orbit vehicles final report of the Collaborative Research Centres 253, 255 and 259 |
| title_auth | Basic research and technologies for Two-Stage-to-Orbit vehicles final report of the Collaborative Research Centres 253, 255 and 259 |
| title_exact_search | Basic research and technologies for Two-Stage-to-Orbit vehicles final report of the Collaborative Research Centres 253, 255 and 259 |
| title_full | Basic research and technologies for Two-Stage-to-Orbit vehicles final report of the Collaborative Research Centres 253, 255 and 259 Deutsche Forschungsgemeinschaft. Ed. by Dieter Jacob ... |
| title_fullStr | Basic research and technologies for Two-Stage-to-Orbit vehicles final report of the Collaborative Research Centres 253, 255 and 259 Deutsche Forschungsgemeinschaft. Ed. by Dieter Jacob ... |
| title_full_unstemmed | Basic research and technologies for Two-Stage-to-Orbit vehicles final report of the Collaborative Research Centres 253, 255 and 259 Deutsche Forschungsgemeinschaft. Ed. by Dieter Jacob ... |
| title_short | Basic research and technologies for Two-Stage-to-Orbit vehicles |
| title_sort | basic research and technologies for two stage to orbit vehicles final report of the collaborative research centres 253 255 and 259 |
| title_sub | final report of the Collaborative Research Centres 253, 255 and 259 |
| topic | Space vehicles Aerodynamics Raumtransporter (DE-588)4177083-3 gnd Technologie (DE-588)4059276-5 gnd Raumfahrttechnik (DE-588)4177061-4 gnd Raumfahrzeug (DE-588)4048579-1 gnd |
| topic_facet | Space vehicles Aerodynamics Raumtransporter Technologie Raumfahrttechnik Raumfahrzeug Aufsatzsammlung |
| url | http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=013140818&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
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