HyShot scramjet testing in the HEG:
Gespeichert in:
| 1. Verfasser: | |
|---|---|
| Format: | Abschlussarbeit Buch |
| Sprache: | English |
| Veröffentlicht: |
Köln
2007
|
| Ausgabe: | Als Ms. gedr. |
| Schriftenreihe: | Forschungsbericht / Deutsches Zentrum für Luft- und Raumfahrt
2007,14 |
| Schlagworte: | |
| Online-Zugang: | Inhaltsverzeichnis |
| Beschreibung: | Getr. Zählung Ill., graph. Darst. 21 cm |
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Datensatz im Suchindex
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| adam_text | FORSCHUNGSBERICHT 2007-14 HYSHOT SCRAMJET TESTING IN THE HEG ANTHONY D.
GARDNER DEUTSCHES ZENTRUM FUR LUFT- UND RAUMFAHRT INSTITUT FUR
AERODYNAMIK UND STROMUNGSTECHNIK GOTTINGEN 302 SEITEN 135 BILDER 60
TABELLEN 126 LITERATURSTELLEN ULB DARMSTADT ILHII DEUTSCHES ZENTRUM DLR
FUR LUFT- UND RAUMFAHRT E.V. IN DER HELMHOLTZ-GEMEINSCHAFT CONTENTS
ACKNOWLEDGMENTS III NOMENCLATURE XXV 1 INTRODUCTION 1 1.1 OVERVIEW OF
THE PROJECT 1 1.1.1 SCRAMJET ENGINES 1 1.1.2 SUPERSONIC COMBUSTION 3
1.1.3 SIMULATION OF HYPERSONIC FLIGHT CONDITIONS . ... 4 1.1.4
EXPERIMENTATION IN SHOCK TUNNELS 6 1.1.5 SUMMARY 8 1.2 ROADMAP FOR THIS
THESIS 9 2 DEVELOPMENT OF A NEW CONDITION FOR THE HEG 11 2.1 THE HIGH
ENTHALPY SHOCK TUNNEL GOTTINGEN 13 2.2 DESIGN OF LOW-ENTHALPY CONDITIONS
15 2.2.1 ANALYTICAL METHOD FOR THE SHOCK AND COMPRESSION TUBES AT BURST
18 2.2.2 ANALYTICAL METHOD FOR THE DRIVER AT LOW ENTHALPY 21 2.2.3 USING
LID FOR COMPLETION AND VERIFICATION OF DE- SIGN 24 2.3 UPGRADES TO THE
HEG 31 2.3.1 THE HEG MACH 8 CONTOURED NOZZLE (NOZZLE III). 31 2.3.2
LUDWIEG TUBE HYDROGEN FUEL SYSTEM 32 2.3.3 DIAPHRAGM STATIC CALIBRATION
AND SELECTION .... 35 2.3.4 DESIGN OF AN 850 KG PISTON WITH BRAKES 38
2.4 CALIBRATION OF THE HEG AT LOW ENTHALPY 49 2.4.1 CONDITION
CALIBRATIONS 50 2.4.2 NOZZLE III CALIBRATIONS , 60 2.4.3 ASSESSMENT OF
PISTON OPERATION 63 2.4.4 HYSHOT INJECTOR CALIBRATION IN HEG 68 2.4.5
SELECTION OF TEST TIME IN THE HEG 70 2.4.6 DETERMINATION OF FREESTREAM
CONDITIONS IN THE HEG 74 2.5 SUMMARY 77 HYSHOT MODEL GROUND TESTING 79
3.1 THE HYSHOT FLIGHT MODEL 80 3.1.1 MODEL GEOMETRY 80 3.1.2
INSTRUMENTATION , 83 3.1.3 FUEL SYSTEM 85 3.2 THE HYSHOT HEG MODEL 86
3.2.1 MODEL GEOMETRY AND FUEL SYSTEM 86 3.2.2 INSTRUMENTATION 90 3.3
HYSHOT MODEL CFD 94 3.3.1 THE DLR-TAU UNSTRUCTURED CODE 94 3.3.2
COMPUTATIONAL GEOMETRY 97 3.3.3 MODELLING EFFECTS 99 3.3.4 EFFECT OF TIP
DECAY 104 3.3.5 TEST CASE FOR SEPARATION CONTROL 106 3.4 TESTS IN THE
HEG 110 3.4.1 FUEL-OFF PRESSURE DATA 112 3.4.2 COMPUTATION OF COMBUSTION
CHAMBER TEMPERATURES/PRESSURES 119 3.4.3 FUEL-OFF HEAT FLUX DATA 120
3.4.4 FUEL INJECTION INTO NITROGEN 124 3.4.5 FUEL INJECTION INTO AIR 133
3.4.6 VARIATION OF EQUIVALENCE RATIO AND ANGLE OF ATTACK 147 3.4.7
BOUNDARY LAYER TRIP AND TEST REPEATABILITY .... 156 3.4.8 DISCUSSION OF
HEG TEST RESULTS . 158 3.5 COMPARISON OF FROST MODEL TESTS IN THE T4 160
3.5.1 THE FROST MODEL 161 3.5.2 METHOD OF COMPARISON WITH HEG DATA 165
3.5.3 TEST CONDITIONS 166 3.5.4 RESULTS AND COMPARISON WITH HEG DATA 167
3.5.5 DISCUSSION 175 3.6 HYSHOT MODEL TESTS IN THE T4 178 3.6.1 MODEL
AND INSTRUMENTATION 178 3.6.2 TEST CONDITIONS 179 3.6.3 COMPARISON OF T4
RESULTS WITH HEG RESULTS . P. 181 3.7 SUMMARY AND CONCLUSION 184 VLL 4
HYSHOT II FLIGHT DATA 185 4.1 SELECTION OF DATA POINTS 188 4.2 FLIGHT
DATA . 192 4.2.1 FUEL-OFF DATA 192 4.2.2 VARIATION OF ANGLE OF ATTACK
197 4.3 COMPARISON WITH GROUND TESTING DATA 201 4.4 SUMMARY AND
CONCLUSION 207 5 CONCLUSION 209 5.1 DESIGN OF NEW CONDITIONS 210 5.1.1
CONCLUSIONS AND RECOMMENDATIONS FOR FUTURE WORK 210 5.2 TESTING OF THE
HYSHOT CONFIGURATION 212 5.2.1 CONCLUSIONS AND RECOMMENDATIONS FOR
FUTURE WORK 212 BIBLIOGRAPHY 217 A FUEL SYSTEM A-L A. 1 FAST ACTING
VALVE DATA SHEETS A-2 A.2 FAST ACTING VALVE DRIVING CIRCUIT A-6 B
DIAPHRAGM CALIBRATION BURST PRESSURES B-L C PISTON DATA C-L C.I STEEL
1.6582 C-2 C.2 STEEL BLANK TEST C-6 C.3 FINISHED PISTON BODY TESTS C-10
C.4 BRAKE MATERIAL DATA SHEET C-12 D NOZZLE CALIBRATION DATA D-L D.I HEG
CONDITIONS XI AND MACH 6, 12KM ALTITUDE D-2 D.2 T4 MACH 7.6 NOZZLE D-4 E
ERROR ANALYSIS FOR HEG CONDITIONS XI AND XII EL F COMPUTATION OF
CONDITIONS AFTER FUEL MIXING F-L
|
| adam_txt |
FORSCHUNGSBERICHT 2007-14 HYSHOT SCRAMJET TESTING IN THE HEG ANTHONY D.
GARDNER DEUTSCHES ZENTRUM FUR LUFT- UND RAUMFAHRT INSTITUT FUR
AERODYNAMIK UND STROMUNGSTECHNIK GOTTINGEN 302 SEITEN 135 BILDER 60
TABELLEN 126 LITERATURSTELLEN ULB DARMSTADT ILHII DEUTSCHES ZENTRUM DLR
FUR LUFT- UND RAUMFAHRT E.V. IN DER HELMHOLTZ-GEMEINSCHAFT CONTENTS
ACKNOWLEDGMENTS III NOMENCLATURE XXV 1 INTRODUCTION 1 1.1 OVERVIEW OF
THE PROJECT 1 1.1.1 SCRAMJET ENGINES 1 1.1.2 SUPERSONIC COMBUSTION 3
1.1.3 SIMULATION OF HYPERSONIC FLIGHT CONDITIONS . . 4 1.1.4
EXPERIMENTATION IN SHOCK TUNNELS 6 1.1.5 SUMMARY 8 1.2 ROADMAP FOR THIS
THESIS 9 2 DEVELOPMENT OF A NEW CONDITION FOR THE HEG 11 2.1 THE HIGH
ENTHALPY SHOCK TUNNEL GOTTINGEN 13 2.2 DESIGN OF LOW-ENTHALPY CONDITIONS
15 2.2.1 ANALYTICAL METHOD FOR THE SHOCK AND COMPRESSION TUBES AT BURST
18 2.2.2 ANALYTICAL METHOD FOR THE DRIVER AT LOW ENTHALPY 21 2.2.3 USING
LID FOR COMPLETION AND VERIFICATION OF DE- SIGN 24 2.3 UPGRADES TO THE
HEG 31 2.3.1 THE HEG MACH 8 CONTOURED NOZZLE (NOZZLE III). 31 2.3.2
LUDWIEG TUBE HYDROGEN FUEL SYSTEM 32 2.3.3 DIAPHRAGM STATIC CALIBRATION
AND SELECTION . 35 2.3.4 DESIGN OF AN 850 KG PISTON WITH BRAKES 38
2.4 CALIBRATION OF THE HEG AT LOW ENTHALPY 49 2.4.1 CONDITION
CALIBRATIONS 50 2.4.2 NOZZLE III CALIBRATIONS , 60 2.4.3 ASSESSMENT OF
PISTON OPERATION 63 2.4.4 HYSHOT INJECTOR CALIBRATION IN HEG 68 2.4.5
SELECTION OF TEST TIME IN THE HEG 70 2.4.6 DETERMINATION OF FREESTREAM
CONDITIONS IN THE HEG 74 2.5 SUMMARY 77 HYSHOT MODEL GROUND TESTING 79
3.1 THE HYSHOT FLIGHT MODEL 80 3.1.1 MODEL GEOMETRY 80 3.1.2
INSTRUMENTATION , 83 3.1.3 FUEL SYSTEM 85 3.2 THE HYSHOT HEG MODEL 86
3.2.1 MODEL GEOMETRY AND FUEL SYSTEM 86 3.2.2 INSTRUMENTATION 90 3.3
HYSHOT MODEL CFD 94 3.3.1 THE DLR-TAU UNSTRUCTURED CODE 94 3.3.2
COMPUTATIONAL GEOMETRY 97 3.3.3 MODELLING EFFECTS 99 3.3.4 EFFECT OF TIP
DECAY 104 3.3.5 TEST CASE FOR SEPARATION CONTROL 106 3.4 TESTS IN THE
HEG 110 3.4.1 FUEL-OFF PRESSURE DATA 112 3.4.2 COMPUTATION OF COMBUSTION
CHAMBER TEMPERATURES/PRESSURES 119 3.4.3 FUEL-OFF HEAT FLUX DATA 120
3.4.4 FUEL INJECTION INTO NITROGEN 124 3.4.5 FUEL INJECTION INTO AIR 133
3.4.6 VARIATION OF EQUIVALENCE RATIO AND ANGLE OF ATTACK 147 3.4.7
BOUNDARY LAYER TRIP AND TEST REPEATABILITY . 156 3.4.8 DISCUSSION OF
HEG TEST RESULTS . 158 3.5 COMPARISON OF FROST MODEL TESTS IN THE T4 160
3.5.1 THE FROST MODEL 161 3.5.2 METHOD OF COMPARISON WITH HEG DATA 165
3.5.3 TEST CONDITIONS 166 3.5.4 RESULTS AND COMPARISON WITH HEG DATA 167
3.5.5 DISCUSSION 175 3.6 HYSHOT MODEL TESTS IN THE T4 178 3.6.1 MODEL
AND INSTRUMENTATION 178 3.6.2 TEST CONDITIONS 179 3.6.3 COMPARISON OF T4
RESULTS WITH HEG RESULTS . P. 181 3.7 SUMMARY AND CONCLUSION 184 VLL 4
HYSHOT II FLIGHT DATA 185 4.1 SELECTION OF DATA POINTS 188 4.2 FLIGHT
DATA . 192 4.2.1 FUEL-OFF DATA 192 4.2.2 VARIATION OF ANGLE OF ATTACK
197 4.3 COMPARISON WITH GROUND TESTING DATA 201 4.4 SUMMARY AND
CONCLUSION 207 5 CONCLUSION 209 5.1 DESIGN OF NEW CONDITIONS 210 5.1.1
CONCLUSIONS AND RECOMMENDATIONS FOR FUTURE WORK 210 5.2 TESTING OF THE
HYSHOT CONFIGURATION 212 5.2.1 CONCLUSIONS AND RECOMMENDATIONS FOR
FUTURE WORK 212 BIBLIOGRAPHY 217 A FUEL SYSTEM A-L A. 1 FAST ACTING
VALVE DATA SHEETS A-2 A.2 FAST ACTING VALVE DRIVING CIRCUIT A-6 B
DIAPHRAGM CALIBRATION BURST PRESSURES B-L C PISTON DATA C-L C.I STEEL
1.6582 C-2 C.2 STEEL BLANK TEST C-6 C.3 FINISHED PISTON BODY TESTS C-10
C.4 BRAKE MATERIAL DATA SHEET C-12 D NOZZLE CALIBRATION DATA D-L D.I HEG
CONDITIONS XI AND MACH 6, 12KM ALTITUDE D-2 D.2 T4 MACH 7.6 NOZZLE D-4 E
ERROR ANALYSIS FOR HEG CONDITIONS XI AND XII EL F COMPUTATION OF
CONDITIONS AFTER FUEL MIXING F-L |
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| dewey-full | 629.134353 |
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| dewey-sort | 3629.134353 |
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| discipline | Maschinenbau / Maschinenwesen Verkehr / Transport |
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| index_date | 2024-07-02T19:31:45Z |
| indexdate | 2024-07-09T21:10:15Z |
| institution | BVB |
| language | English |
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| physical | Getr. Zählung Ill., graph. Darst. 21 cm |
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| spelling | Gardner, Anthony D. Verfasser aut HyShot scramjet testing in the HEG Anthony D. Gardner Als Ms. gedr. Köln 2007 Getr. Zählung Ill., graph. Darst. 21 cm txt rdacontent n rdamedia nc rdacarrier Forschungsbericht / Deutsches Zentrum für Luft- und Raumfahrt 2007,14 Zugl.: Brisbane, Univ. of Queensland, Diss., 2007 Flugversuch (DE-588)4196196-1 gnd rswk-swf Stoßwellenrohr (DE-588)4183445-8 gnd rswk-swf Überschallstaustrahltriebwerk (DE-588)4427457-9 gnd rswk-swf Gasströmung (DE-588)4156052-8 gnd rswk-swf (DE-588)4113937-9 Hochschulschrift gnd-content Flugversuch (DE-588)4196196-1 s Stoßwellenrohr (DE-588)4183445-8 s Überschallstaustrahltriebwerk (DE-588)4427457-9 s Gasströmung (DE-588)4156052-8 s DE-604 Deutsches Zentrum für Luft- und Raumfahrt Forschungsbericht 2007,14 (DE-604)BV011758990 2007,14 HEBIS Datenaustausch Darmstadt application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=016271138&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
| spellingShingle | Gardner, Anthony D. HyShot scramjet testing in the HEG Flugversuch (DE-588)4196196-1 gnd Stoßwellenrohr (DE-588)4183445-8 gnd Überschallstaustrahltriebwerk (DE-588)4427457-9 gnd Gasströmung (DE-588)4156052-8 gnd |
| subject_GND | (DE-588)4196196-1 (DE-588)4183445-8 (DE-588)4427457-9 (DE-588)4156052-8 (DE-588)4113937-9 |
| title | HyShot scramjet testing in the HEG |
| title_auth | HyShot scramjet testing in the HEG |
| title_exact_search | HyShot scramjet testing in the HEG |
| title_exact_search_txtP | HyShot scramjet testing in the HEG |
| title_full | HyShot scramjet testing in the HEG Anthony D. Gardner |
| title_fullStr | HyShot scramjet testing in the HEG Anthony D. Gardner |
| title_full_unstemmed | HyShot scramjet testing in the HEG Anthony D. Gardner |
| title_short | HyShot scramjet testing in the HEG |
| title_sort | hyshot scramjet testing in the heg |
| topic | Flugversuch (DE-588)4196196-1 gnd Stoßwellenrohr (DE-588)4183445-8 gnd Überschallstaustrahltriebwerk (DE-588)4427457-9 gnd Gasströmung (DE-588)4156052-8 gnd |
| topic_facet | Flugversuch Stoßwellenrohr Überschallstaustrahltriebwerk Gasströmung Hochschulschrift |
| url | http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=016271138&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
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