81–100 von 160 Ergebnissen
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    SUPERSONIC COMBUSTION PROCESSES IN A PREMIXED 3D NON-UNIFORM-COMPRESSION SCRAMJET ENGINE

    Bricalli, M.G. / Boyce, R.R. / Brown, L. et al. | British Library Conference Proceedings | 2012

    EXPERIMENTAL STUDY ON THE APPLICABILITY OF LASER-INDUCED GRATING SPECTROSCOPY FOR TEMPERATURE MEASUREMENTS IN SHOCK TUNNELS AND SHOCK TUBES

    Sander, T. / Altenhofer, P. / Mundt, C. et al. | British Library Conference Proceedings | 2012

    RESEARCH ON HOT GAS JET IGNITION PROCESS OF SCRAMJET COMBUSTOR FUELED WITH KEROSENE

    Li, Q. / Wenxiong, X. / Lin, L. et al. | British Library Conference Proceedings | 2012

    THE SEPARATION PATTERN TRANSITION PHENOMENA AND ITS EFFECTS ON THE SERN PERFORMANCE

    Yu, Y. / Xu, J. / Wang, M. et al. | British Library Conference Proceedings | 2012

    CFD ANALYSIS OF UNSTEADY COMBUSTION PHENOMENA IN THE HYSHOT-II SCRAMJET CONFIGURATION

    Karl, S. / Laurence, S. / Schramm, J.M. et al. | British Library Conference Proceedings | 2012

    SENSITIVITY OF FLIGHT DYNAMICS OF HYPERSONIC VEHICLES TO DESIGN PARAMETERS

    Dalle, D.J. / Torrez, S.M. / Driscoll, J.F. et al. | British Library Conference Proceedings | 2012

    SHOCK TUNNEL AND NUMERICAL STUDIES OF A LARGE INLET-FUELLED INWARD TURNING AXISYMMETRIC SCRAMJET

    Boyce, R.R. / Schramm, J.M. / Oberg, D. et al. | British Library Conference Proceedings | 2012

    RADICAL CLEARANCE ANALYSIS ON THE HIGH PRESSURE COMPRESSOR

    Yu, Y. / Liu, Q. / Shen, B. et al. | British Library Conference Proceedings | 2012

    EXPERIMENTAL INVESTIGATION OF HYPERSONIC BOUNDARY-LAYER STABILIZATION ON A CONE BY MEANS OF ULTRASONICALLY ABSORPTIVE CARBON-CARBON MATERIAL

    Wagner, A. / Hannemann, K. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2012

    THE AEROTHERMAL, THERMAL AND STRUCTURAL DESIGN PROCESS AND CRITERIA FOR THE HIFIRE-4 FLIGHT TEST VEHICLE

    Lau, K.Y. / Woo, Y. / Tran, J. et al. | British Library Conference Proceedings | 2012

    MODELING, ANALYSIS AND OPTIMIZATION OF THE AIR-TURBOROCKET EXPANDER ENGINE

    Miranda, I.R. / Villace, V.F. / Paniagua, G. et al. | British Library Conference Proceedings | 2012

    COMBUSTION SCALING IN AN INLET INJECTION SCRAMJET

    Schloegel, F. / Boyce, R.R. / McIntyre, T.J. et al. | British Library Conference Proceedings | 2012

    MULTIDISCIPLINARY OPTIMIZATION OF STARBODY WAVERIDER SHAPES FOR LIFTING AEROCAPTURE WITH ORBITAL PLANE CHANGE

    Knittel, J. / Lewis, M. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2012

    FUEL ATOMIZATION AND DROPLET BREAKUP MODELS FOR NUMERICAL SIMULATION OF SPRAY COMBUSTION IN A SCRAMJET COMBUSTOR

    Yang, S. / Le, J. / He, W. et al. | British Library Conference Proceedings | 2012

    ISO-CONTRACTION-RATIO METHODOLOGY FOR THE DESIGN OF HYPERSONIC INWARD TURNING INLETS WITH SHAPE TRANSITION

    Xiao, Y. / Yue, L. / Chenr, L. et al. | British Library Conference Proceedings | 2012

    DYNAMIC INVERSION-BASED CONTROL SYSTEM OF A HYPERSONIC VEHICLE WITH MODEL UNCERTAINTY

    Wan, J. / Wang, Q. / Ai, J. et al. | British Library Conference Proceedings | 2012

    WAKE FLOW CONTROL ON THE AFTERBURNER BEHIND FUEL INJECTION AND FLAME HOLDING STRUT FOR HYPERSONIC VEHICLE

    Araki, S. / Sakaue, S. / Arai, T. et al. | British Library Conference Proceedings | 2012

    ASSESSMENT OF A PARTIALLY STIRRED REACTOR COMBUSTION MODEL TO PREDICT THE LEAN BLOW-OUT LIMIT OF A RAMJET COMBUSTOR

    Le Pichon, T. / Sabel Nikov, V. / Moule, Y. et al. | British Library Conference Proceedings | 2012

    THREE-DIMENSIONAL CHARACTERISTICS AND CONTROL METHOD OF SHOCK/BOUNDARY LAYER INTERACTIONS IN A DUCT WITH FINITE WIDTH

    Zhang, Y. / Tan, H.-J. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2012

    EXPERIMENTAL STUDY ON THE AERODYNAMIC PERFORMANCE OF CLUSTERED LINEAR AEROSPIKE NOZZLES

    Takahashi, H. / Tomioka, S. / Sakuranaka, N. et al. | British Library Conference Proceedings | 2012