Analysis of a Pulsed Normal Detonation Wave Engine Concept (English)
- New search for: Wilson, D.
- New search for: Lu, F.
- New search for: Kim, H.
- New search for: Munipalli, R.
- New search for: American Institute of Aeronautics and Astronautics
- New search for: Wilson, D.
- New search for: Lu, F.
- New search for: Kim, H.
- New search for: Munipalli, R.
- New search for: American Institute of Aeronautics and Astronautics
In:
Space planes and hypersonic systems and technologies
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161-171
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2001
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ISBN:
- Conference paper / Print
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Title:Analysis of a Pulsed Normal Detonation Wave Engine Concept
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Contributors:Wilson, D. ( author ) / Lu, F. ( author ) / Kim, H. ( author ) / Munipalli, R. ( author ) / American Institute of Aeronautics and Astronautics
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Conference:International conference; 10th, Space planes and hypersonic systems and technologies ; 2001 ; Kyoto, Japan
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Published in:
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Publisher:
- New search for: AIAA
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Publication date:2001-01-01
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Size:11 pages
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Remarks:Contains papers AIAA-2001-1750 to 1927 only with gaps
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ISBN:
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Type of media:Conference paper
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Type of material:Print
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Language:English
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Keywords:
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Source:
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Table of contents conference proceedings
The tables of contents are generated automatically and are based on the data records of the individual contributions available in the index of the TIB portal. The display of the Tables of Contents may therefore be incomplete.
- 1
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Numerical Solution of Hypersonic Compression Corner FlowsDogrusoz, S. / Kavsaoglu, M. / Kaynak, U. / American Institute of Aeronautics and Astronautics et al. | 2001
- 11
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Prediction of Hypersonic Shock/Shock Interaction Heating Using Hybrid Adaptive Unstructured GridsMiyaji, K. / American Institute of Aeronautics and Astronautics et al. | 2001
- 18
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On the Performance of Upwind Schemes and Turbulence Models in Hypersonic FlowsCoratekin, T. / VanKeuk, J. / Ballmann, J. / American Institute of Aeronautics and Astronautics et al. | 2001
- 34
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Experimental and Computational Investigation of Supersonic Cavity FlowsZhang, J. / Morishita, E. / Okunuki, T. / Itoh, H. / American Institute of Aeronautics and Astronautics et al. | 2001
- 45
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Detection of Shock Motion using Laser Schlieren System in a Hypersonic SWBLI FlowfieldVerma, S. / Koppenwallner, G. / American Institute of Aeronautics and Astronautics et al. | 2001
- 53
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PIV Measurements in a Mach 2 Hydrogen-Air Supersonic CombustionWeisgerber, H. / Martinuzzi, R. / Brummund, U. / Magre, P. / American Institute of Aeronautics and Astronautics et al. | 2001
- 64
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OH/Acetone PLIF and CARS Thermometry in a Supersonic Reactive LayerBresson, A. / Bouchardy, P. / Magre, P. / Grisch, F. / American Institute of Aeronautics and Astronautics et al. | 2001
- 75
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Angled Injection through Diamond-Shaped Orifices into a Supersonic StreamTomioka, S. / Jacobsen, L. / Schetz, J. / American Institute of Aeronautics and Astronautics et al. | 2001
- 87
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Ignition by an H2/O2-Microburner in a Supersonic AirflowKobayashi, K. / Tomioka, S. / Mitani, T. / American Institute of Aeronautics and Astronautics et al. | 2001
- 96
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Experiments on Flame Holding Position of the Fin-less Projectile in Ram AcceleratorYatsufusa, T. / Chang, X. / Taki, S. / American Institute of Aeronautics and Astronautics et al. | 2001
- 105
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An Integrated Aeroramp-Injector/Plasma Igniter for Hydrocarbon Fuels in Supersonic Flow - Part A: Experimental Studies of the Geometric ConfigurationJacobsen, L. / Gallimore, S. / Schetz, J. / O Brien, W. / Goss, L. / American Institute of Aeronautics and Astronautics et al. | 2001
- 118
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An Integrated Aeroramp-Injector/Plasma-Igniter for Hydrocarbon Fuels in Supersonic Flow - Part B: Experimental Studies of the Operating ConditionsGallimore, S. / Jacobsen, L. / O Brien, W. / Schetz, J. / American Institute of Aeronautics and Astronautics et al. | 2001
- 128
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The Direct Measurement of Friction in the Boundary Layer at Supersonic Flow VelocitiesGoldfeld, M. / Petrochenko, V. / Nestoulia, R. / Shishov, V. / Falempin, F. / American Institute of Aeronautics and Astronautics et al. | 2001
- 135
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Hydrogen Concentration Measurements of Supersonic Hydrogen-Air Shear Layer using Catalytic ReactionArai, T. / Kasahara, J. / Sakima, F. / Miura, J. / Ami, T. / Nagata, H. / American Institute of Aeronautics and Astronautics et al. | 2001
- 141
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Oxidation Behavior of CVD-SiC in High Temperature AtmosphereWakamatsu, Y. / Ono, F. / Saito, T. / American Institute of Aeronautics and Astronautics et al. | 2001
- 148
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Thermal Response and Oxidation Behavior of Si-Ti-C-O Fiber/Si-Ti-C-O Ceramic Matrix Composites under Atmospheric Re-entry ConditionsOgasawara, T. / Ishikawa, T. / Matsuzaki, T. / American Institute of Aeronautics and Astronautics et al. | 2001
- 155
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HOPE-X All-Composite Prototype StructureAsada, S. / Nishiwaki, K. / Niitsu, M. / Yamamoto, T. / Kamita, T. / Kimura, G. / American Institute of Aeronautics and Astronautics et al. | 2001
- 161
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Analysis of a Pulsed Normal Detonation Wave Engine ConceptWilson, D. / Lu, F. / Kim, H. / Munipalli, R. / American Institute of Aeronautics and Astronautics et al. | 2001
- 172
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A Pulsed Detonation Based Multimode Engine ConceptMunipalli, R. / Shankar, V. / Wilson, D. / Kim, H. / Lu, F. / Hagseth, P. / American Institute of Aeronautics and Astronautics et al. | 2001
- 182
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Determination of the Integral and Local Characteristics of Supersonic Pulsed Detonation Ramjet Engine (SPDRE)Alexandrov, V. / Kraiko, A. / Reent, K. / American Institute of Aeronautics and Astronautics et al. | 2001
- 193
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Mission Safety Concept for a Two-Stage Space Transportation VehicleMayrhofer, M. / Sachs, G. / American Institute of Aeronautics and Astronautics et al. | 2001
- 201
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Conceptual Design of Two-Stage Reusable Launch Systems using X-33Sawada, K. / Takashi, M. / American Institute of Aeronautics and Astronautics et al. | 2001
- 210
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A Two-Stage-to-Orbit Spaceplane Concept with Growth PotentialMehta, U. / Bowles, J. / American Institute of Aeronautics and Astronautics et al. | 2001
- 231
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Study on Flowfield Around Space Plane Traveling at Mach 10Manabe, K. / Nishio, M. / Sezaki, S. / American Institute of Aeronautics and Astronautics et al. | 2001
- 238
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Optimum Three-Dimensional Hypersonic Bodies within the Framework of a Local Interaction ModelYakunina, G. / American Institute of Aeronautics and Astronautics et al. | 2001
- 248
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Experimental Investigations of Steady-State Oblique Detonation Waves Generated around Hypersonic ProjectilesKasahara, J. / Arai, T. / Matsuo, A. / Akai, N. / Takazawa, K. / American Institute of Aeronautics and Astronautics et al. | 2001
- 256
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Hyper-X Stage Separation - Simulation Development and ResultsReubush, D. / Martin, J. / Robinson, J. / Bose, D. / Strovers, B. / American Institute of Aeronautics and Astronautics et al. | 2001
- 263
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Hope-X High Speed Flight Demonstration Program Phase IIYanagihara, M. / Miyazawa, Y. / Akimoto, T. / Sagisaka, M. / Cretenet, J.-C. / Venel, S. / American Institute of Aeronautics and Astronautics et al. | 2001
- 269
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HOPE-X High Speed Flight Demonstration Program Phase ISato, N. / Akimoto, T. / Miyazawa, Y. / American Institute of Aeronautics and Astronautics et al. | 2001
- 274
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The Prospects of Hypersonic Engines In-Flight Testing Technology DevelopmentRoudakov, A. / Semenov, V. / Strokin, M. / Relin, V. / Tsyplakov, V. / Kondratov, A. / American Institute of Aeronautics and Astronautics et al. | 2001
- 279
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Investigation of Flowfield Around Hypersonic Re-entry Capsule Utilizing the Electric Discharge MethodNishio, M. / Manabe, K. / Sezaki, S. / American Institute of Aeronautics and Astronautics et al. | 2001
- 288
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Hyper-X Flight Engine Ground Testing for X-43 Flight Risk ReductionHuebner, L. / Rock, K. / Ruf, E. / Witte, D. / Andrews, E. / American Institute of Aeronautics and Astronautics et al. | 2001
- 302
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Experimental Study of Wake behind Hypersonic Vehicle Utilizing the Electric Discharge MethodNishio, M. / Nakamura, H. / Sezaki, S. / American Institute of Aeronautics and Astronautics et al. | 2001
- 308
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Wind Tunnel Tests for Separation Dynamics Modeling of a Two-Stage Hypersonic VehicleBreitsamter, C. / Laschka, B. / ZShringer, C. / Sachs, G. / American Institute of Aeronautics and Astronautics et al. | 2001
- 318
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Integrated System Test of an Airbreathing Rocket (ISTAR)Faulkner, R. / American Institute of Aeronautics and Astronautics et al. | 2001
- 329
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Staging Evaluation of a Two-Stage-To-Orbit Vehicle at Mach 8Wingfield, L. / American Institute of Aeronautics and Astronautics et al. | 2001
- 339
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Dual-Mode Operation in a Scramjet CombustorKanda, T. / Chinzei, N. / Kudo, K. / Murakami, A. / American Institute of Aeronautics and Astronautics et al. | 2001
- 347
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Computational Analysis of a Kerosene-Fueled ScramjetDufour, E. / Bouchez, M. / American Institute of Aeronautics and Astronautics et al. | 2001
- 358
-
Application of OH Radical Radiation for Determination of Kerosene Combustion EfficiencyGoldfeld, M. / Mironov, S. / Mishunin, A. / Potapkin, A. / American Institute of Aeronautics and Astronautics et al. | 2001
- 367
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Numerical and Experimental Investigation of Supersonic Mixing and CombustionGouskov, O. / Kopchenov, V. / Lomkov, K. / Mnatsakanyan, Y. / Prokhorov, A. / Shutov, A. / American Institute of Aeronautics and Astronautics et al. | 2001
- 377
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Aerothermal Performance Constraints for Small Radius Nosetip at High AltitudeLee, C. / Park, S. / American Institute of Aeronautics and Astronautics et al. | 2001
- 386
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Thermal Protection and Drag Reduction with Use of Spike in Hypersonic FlowMotoyama, N. / Mihara, K. / Miyajima, R. / Watanuki, T. / Kubota, H. / American Institute of Aeronautics and Astronautics et al. | 2001
- 392
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Study on Trajectory Optimization of Space Plane Ascending to ISSYokoyama, N. / Suzuki, S. / Tsuchiya, T. / American Institute of Aeronautics and Astronautics et al. | 2001
- 400
-
IMM Based Jamming Detection in a DGPS-Aided Inertial SystemChen, G. / Harigae, M. / American Institute of Aeronautics and Astronautics et al. | 2001
- 409
-
Guidance and Control Design for HOPE-X High Speed Flight Demonstrator Phase IITsukamoto, T. / Suzuki, H. / Sagisaka, M. / Nishizawa, T. / American Institute of Aeronautics and Astronautics et al. | 2001
- 418
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Flight Dynamics Modeling Environment for Controller Design and Analysis of Hypersonic VehiclesHolzapfel, F. / Heller, M. / Zahringer, C. / Sachs, G. / American Institute of Aeronautics and Astronautics et al. | 2001
- 429
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Application of Mahalanobis Taguchi System to Fault Diagnosis for Future SpacecraftMatsuda, R. / Ikeda, Y. / Kamoshita, T. / Touhara, K. / American Institute of Aeronautics and Astronautics et al. | 2001
- 438
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Stability and Control Analysis of a Wave-Rider TSTO Second StageJohnson, D. / Thomas, R. / Manor, D. / American Institute of Aeronautics and Astronautics et al. | 2001
- 447
-
A Feasibility Study of an ATREX Engine at Approved Technology LevelsIsomura, K. / Omi, J. / Murooka, T. / Tanatsugu, N. / Sato, T. / American Institute of Aeronautics and Astronautics et al. | 2001
- 454
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Development Study of the ATREX Engine for TSTO SpaceplaneSato, T. / Tanatsugu, N. / Hatta, H. / Goto, K. / Kobayashi, H. / Omi, J. / American Institute of Aeronautics and Astronautics et al. | 2001
- 463
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The SSTO Combined Propulsion System on a Basis of LACEC and DMSCRJDulepov, N. / Lanshin, A. / Tjurikov, E. / Smolyarov, V. / American Institute of Aeronautics and Astronautics et al. | 2001
- 470
-
The Themis Launch Vehicle: the Definitive Demonstration Prior to Future European RLVDelattre, N. / Clar, P. / Deneu, F. / Malassigne, M. / American Institute of Aeronautics and Astronautics et al. | 2001
- 479
-
Design and Analysis of Payload-Optimized WaveridersLobbia, M. / Suzuki, K. / American Institute of Aeronautics and Astronautics et al. | 2001
- 489
-
Simulation of an Orbiter Separation Maneuver at Hypersonic SpeedCvrlje, T. / Laschka, B. / American Institute of Aeronautics and Astronautics et al. | 2001
- 500
-
Three-Dimensional DSMC Simulation of Hypersonic Rarefied Gas Flow Around a Sharp Flat PlateTsuboi, N. / Yamaguchi, H. / Matsumoto, Y. / American Institute of Aeronautics and Astronautics et al. | 2001
- 509
-
Unsteady Aerodynamics of a Hypersonic Vehicle during a Separation PhaseDecker, K. / Laschka, B. / American Institute of Aeronautics and Astronautics et al. | 2001
- 520
-
A New Method for Improved Flow Simulation at High Mach NumbersHakkinen, R. / American Institute of Aeronautics and Astronautics et al. | 2001
- 524
-
Hypersonic Flow Generation and Diagnostics in Expansion TubeSasoh, A. / Ohnishi, Y. / Ramjaun, D. / Takayama, K. / American Institute of Aeronautics and Astronautics et al. | 2001
- 531
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Experimental Study on Flowfield Around Hypersonic Space Plane Utilizing the Electric Discharge MethodNishio, M. / Kai, K. / Sezaki, S. / American Institute of Aeronautics and Astronautics et al. | 2001
- 536
-
RAPIERE: An Innovative Industrial Optical Measurement System for Scramjet FlowsBouchez, M. / Legras, O. / Vallet, I. / Gokalp, I. / Deizarra, C. / Herve, P. / American Institute of Aeronautics and Astronautics et al. | 2001
- 544
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Test Technology Development and Demonstration for Hypersonic Aeropropulsion SystemsGarrard, D. / Bates, L. / American Institute of Aeronautics and Astronautics et al. | 2001
- 552
-
Computational Analysis of the Flow Field near the Boat-tail Region of Annular Plug NozzlesFujii, K. / Imai, K. / Sato, T. / American Institute of Aeronautics and Astronautics et al. | 2001
- 561
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Computation of the Expansion Flow of a Hypersonic Propulsion SystemLink, T. / Koschel, W. / American Institute of Aeronautics and Astronautics et al. | 2001
- 572
-
NASA's Spaceliner Investment Area Technology ActivitiesHueter, U. / American Institute of Aeronautics and Astronautics et al. | 2001
- 580
-
The French PROMETHEE Program on Hydrocarbon Fueled Dual Mode Ramjet Status in 2001Serre, L. / Falempin, F. / American Institute of Aeronautics and Astronautics et al. | 2001
- 589
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French-Russian Partnership on Hypersonic Wide Range Ramjets: Status in 2001Bouchez, M. / Falempin, F. / Levine, V. / Avrashkov, V. / Davidenko, D. / American Institute of Aeronautics and Astronautics et al. | 2001
- 600
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The Program for the Complex Investigation of the Hypersonic Flight Laboratory (HFL) "Igla" in the PGU of TSNIIMASHKislykh, V. / Kondratov, A. / Semenov, V. / American Institute of Aeronautics and Astronautics et al. | 2001
- 611
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Material Research on Reusable Launch Vehicles at NAL/KRCKumakawa, A. / Moriya, S. / Niino, M. / Yoshida, M. / Nosaka, M. / Watanabe, Y. / American Institute of Aeronautics and Astronautics et al. | 2001
- 620
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Overview of Basic Research Activities on Cryogenic Composite Propellant Tanks in JapanAoki, T. / Ishikawa, T. / Morino, Y. / American Institute of Aeronautics and Astronautics et al. | 2001
- 629
-
Overview of Development Activities of Spaceplane Components using NUSK-CMC (CMC with Continuous Si-Ti-C-O Fiber)Ishikawa, T. / Ogasawara, T. / American Institute of Aeronautics and Astronautics et al. | 2001
- 639
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An Innovative Technology for Fuel-Cooled Composite Materials StructureFalempin, F. / Bouchez, M. / Salmon, T. / Lespade, P. / Avrashkov, V. / American Institute of Aeronautics and Astronautics et al. | 2001
- 648
-
Lessons Learned from HOPE System DesigningAsada, S. / Miyake, S. / Kouchiyama, J. / Akimoto, T. / Shirouzu, M. / American Institute of Aeronautics and Astronautics et al. | 2001
- 653
-
MHD Flight Control System for Hypersonic VehiclesRobinson, W. / Gerwin, R. / American Institute of Aeronautics and Astronautics et al. | 2001
- 664
-
Evaluation of Internal Aerodynamic Performance in Scramjet EnginesMitani, T. / Kobayashi, K. / Hiraiwa, T. / Tomioka, S. / Masuya, G. / American Institute of Aeronautics and Astronautics et al. | 2001
- 672
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Tests of the Japhar Dual Mode Ramjet EngineDessornes, O. / Scherrer, D. / Novelli, P. / American Institute of Aeronautics and Astronautics et al. | 2001
- 680
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Unstart Phenomenon due to Thermal Choke in Scramjet ModuleMashio, S. / Kurashina, K. / Bamba, T. / Okimoto, S. / Kaji, S. / American Institute of Aeronautics and Astronautics et al. | 2001
- 687
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Turbulent Hypervelocity Fuel/Air Mixing by Cantilevered Ramp InjectorsParent, B. / Sislian, J. / American Institute of Aeronautics and Astronautics et al. | 2001
- 698
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Design and Experimental Evaluation of a Mach 2-Mach 8 InletFalempin, F. / Goldfeld, M. / American Institute of Aeronautics and Astronautics et al. | 2001
- 705
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Trailing Edge Cavity Afterbodies for Linear Plug Nozzle EnginesWisse, M. / Bannink, W. / American Institute of Aeronautics and Astronautics et al. | 2001
- 714
-
Corrugated and Composite Nozzle-Inlets for Thrust and Noise BenefitsGilinsky, M. / Blankson, I. / Gromov, V. / Sakharov, V. / American Institute of Aeronautics and Astronautics et al. | 2001
- 725
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Development Study on Axisymmetric Air Inlet for ATREX EngineKojima, T. / Tanatsuga, N. / Sato, T. / Kanda, M. / Enomoto, Y. / American Institute of Aeronautics and Astronautics et al. | 2001
- 733
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First Stage Design Variations of Partially Reusable Launch VehiclesSippel, M. / Atanassov, U. / Klevanski, I. / Schmid, V. / American Institute of Aeronautics and Astronautics et al. | 2001
- 744
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Magnetohydrodynamic Energy Bypass Applications for Single Stage-to-Orbit VehiclesLee, Y.-M. / Czysz, P. / Petley, D. / American Institute of Aeronautics and Astronautics et al. | 2001
- 754
-
The X-15 as an Analog to Expected Experimental Vehicle Operations and CostsSpringer, A. / American Institute of Aeronautics and Astronautics et al. | 2001
- 765
-
Reentry Environment Advanced Diagnostics (READ) Flight Experiment on USERS Reentry VehicleAbe, T. / Fujita, K. / Otsu, H. / Hama, K. / Shingu, S. / Ichizono, K. / American Institute of Aeronautics and Astronautics et al. | 2001
- 773
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Flight Evaluation of GN&C System and Vertical Landing Dynamics of Reusable Rocket VehicleYamakawa, H. / Higuchi, K. / Maruyama, T. / Kubota, N. / American Institute of Aeronautics and Astronautics et al. | 2001
- 784
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North European Aerospace Test Range - NEATAbrahamsson, M. / Lundahl, K. / American Institute of Aeronautics and Astronautics et al. | 2001
- 790
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Hyper-X Program StatusMcClinton, C. / Rausch, D. / Sitz, J. / Reukauf, P. / American Institute of Aeronautics and Astronautics et al. | 2001
- 802
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Combined Engine for a Reusable Launch Vehicle (KLIN Cycle)Balepin, V. / Czysz, P. / Moszee, R. / American Institute of Aeronautics and Astronautics et al. | 2001
- 813
-
Optimization of Airbreathing Propulsion System for the TSTO SpaceplaneKobayashi, H. / Sato, T. / Tanatsugu, N. / American Institute of Aeronautics and Astronautics et al. | 2001
- 822
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Propulsion Systems for TSTO Airplane-Accelerators of Different TypesDulepov, N. / Lanshin, A. / Sokolova, O. / Tjurikov, E. / American Institute of Aeronautics and Astronautics et al. | 2001
- 833
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Fundamental Techniques of the "Ajax" Concept. Modern State of ResearchKuranov, A. / Korabelnicov, A. / Kuchinskiy, V. / Sheikin, E. / American Institute of Aeronautics and Astronautics et al. | 2001
- 843
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Dual-Mode Ramjet Thermo-Mechanical Design and Associated PerformanceBouchez, M. / American Institute of Aeronautics and Astronautics et al. | 2001
- 852
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Multidisciplinary Design Optimization of a Re-Entry Vehicle Shape and TrajectoryTava, M. / Suzuki, S. / American Institute of Aeronautics and Astronautics et al. | 2001
- 861
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Design Studies of the JAPHAR Experimental Vehicle for Dual Mode Ramjet DemonstrationEggers, T. / Novelli, P. / Haupt, M. / American Institute of Aeronautics and Astronautics et al. | 2001
- 871
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Maglev for Space Launchersdel Monte, L. / Gamma, F. / Andriani, R. / American Institute of Aeronautics and Astronautics et al. | 2001
- 878
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Interactions Between Propulsion Systems and the Configuration Concepts Defines the Design SpaceCzysz, P. / Bruno, C. / Kato, K. / American Institute of Aeronautics and Astronautics et al. | 2001
- 898
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A Concept of Partially Reusable Omniazimuth Aviation-Space Rocket Carrier using the Same Take-Off and Landing SiteKostromin, S. / Sokolov, Y. / Sobolevski, V. / American Institute of Aeronautics and Astronautics et al. | 2001
- 905
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Configuration Development for a Hydrocarbon Fueled Hypersonic Cruise VehicleJohnson, D. / Bogar, T. / Hunt, J. / American Institute of Aeronautics and Astronautics et al. | 2001
- 911
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Scramjet Development and Testing in the United StatesAndrews, E. / American Institute of Aeronautics and Astronautics et al. | 2001