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    NUMERICAL INVESTIGATIONS OF INLET-COMBUSTOR INTERACTIONS FOR A SCRAMJET HYDROGEN-FUELED ENGINE AT A MACH FLIGHT NUMBER OF 8

    Santana, E.R. / Weigand, B. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2012

    THERMAL TESTING OF THE SHARP LEADING EDGE OF SHEFEXII

    Bohrk, H. / Dittert, C. / Weihs, H. et al. | British Library Conference Proceedings | 2012

    INJECTORS AND COMBUSTION PERFORMANCE OF ROCKET THRUSTER FOR ROCKET-RAMJET COMBINED-CYCLE ENGINE MODEL

    Takegoshi, M. / Tomioka, S. / Ono, F. et al. | British Library Conference Proceedings | 2012

    NUMERICAL SIMULATIONS OF NONEQUILIBRIUM FLOWS OVER ROUNDED MODELS AT REENTRY SPEEDS

    Wen, C.-Y. / Massimi, H.S. / Chen, Y.-S. et al. | British Library Conference Proceedings | 2012

    A KALMAN-FILTER BASED INERTIAL NAVIGATION SYSTEM PROCESSOR FOR THE SCRAMSPACE 1 HYPERSONIC FLIGHT EXPERIMENT

    Creagh, M.A. / Beasley, P. / Dimitrijevic, I. et al. | British Library Conference Proceedings | 2012

    DESIGN OF A CIRCULAR TO RECTANGULAR TRANSITION SCRAMJET NOZZLE WITH STREAMLINE TRACING TECHNIQUE

    Mo, J. / Xu, J. / Gu, R. et al. | British Library Conference Proceedings | 2012

    TECHNOLOGY STATUS OF FUEL COOLED CERAMIC MATRIX COMPOSITES FOR DUAL-MODE RAMJET (DMR) AND LIQUID ROCKET ENGINE (LRE) APPLICATIONS

    Beyer, S. / Schmidt-Wimmer, S. / Quering, K. et al. | British Library Conference Proceedings | 2012

    FOCUSING-SCHLIEREN VISUALIZATION IN DIRECT-CONNECT DUAL-MODE SCRAMJET

    Kouchi, T. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2012

    A DYNAMICS STUDY FOR THE HOT STAGE SEPARATION OF A MULTISTAGE ROCKET WITH A COUPLED CFD FLIGHT MECHANICS APPROACH

    Li, Y. / Eggers, T. / Reimann, B. et al. | British Library Conference Proceedings | 2012

    INSTRUMENTATION OF THE SHEFEX-II FLIGHT EXPERIMENT AND SELECTED FLIGHT DATA

    Gulhan, A. / Siebe, F. / Thiele, T. et al. | British Library Conference Proceedings | 2012

    RESEARCH ON THE COMBINED HEATING METHOD USING DUAL SUBSONIC GAS FLOW OF HIGH AND MIDDLE TEMPERATURE FOR THERMAL TEST OF TIP WEDGE STRUCTURE

    Dong, S. / Li, Z. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2012

    HYPERSONIC AEROELASTIC STABILITY BOUNDARY COMPUTATIONS USING RADIAL BASIS FUNCTIONS FOR MESH DEFORMATION

    Lamorte, N. / Friedmann, P.P. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2012

    STRUCTURAL DESIGN AND OPTIMISATION OF THE LAPCAT A2 MACH 5 VEHICLE BASED ON AERO-ELASTIC DEFORMATIONS

    Sharifzadeh, S. / Hendrick, P. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2012

    THE UNSTEADY FLOW PHYSICS OF HYPERSONIC INLET STARTING PROCESSES

    Grainger, A.L. / Boyce, R.R. / Tirtey, S.C. et al. | British Library Conference Proceedings | 2012

    NUMERICAL ANALYSIS OF SCRAMJET MODE OPERATION OF A RBCC ENGINE

    Kodera, M. / Tomioka, S. / Ueda, S. et al. | British Library Conference Proceedings | 2012

    APPLICATION OF THE FADS SYSTEM TO HYPERSONIC FLIGHT VEHICLES WITH SHARP WEDGED FORE-BODIES

    Wang, P. / Jin, X. / Zhao, X.-J. et al. | British Library Conference Proceedings | 2012

    GNC REQUIREMENTS OF FOR A LONG RANGE HYPERSONIC TRANSPORT SYSTEM

    Haya-Ramos, R. / De Zaiacomo, G. / Freixa, J. et al. | British Library Conference Proceedings | 2012

    PRESENT STATUS AND PROSPECTS OF JAXA'S RESEARCH ON FUTURE SPACE TRANSPORTATION SYSTEM

    Fujii, K. / Ishimoto, S. / Mugitani, T. et al. | British Library Conference Proceedings | 2012

    THE SCRAMSPACE I SCRAMJET FLIGHT EXPERIMENT DESIGN AND CONSTRUCTION

    Tirtey, S.C. / Boyce, R.R. / Brown, L.M. et al. | British Library Conference Proceedings | 2012