121–140 von 160 Ergebnissen
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    DEVELOPING AN EMOTIONAL INTELLIGENT CONTROLLER FOR SPACE LAUNCH VEHICLE APPLICATION

    Mohammadi, A. / Tayefi, M. / Ebrahimi, M. et al. | British Library Conference Proceedings | 2012

    DESIGN OPTIMIZATION IN HYPERSONIC FLOWS

    Eyi, S. / Yumusak, M. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2012

    DESIGN OF AN AIRFRAME INTEGRATED 3D SCRAMJET AND EXPERIMENTAL RESULTS AT A MACH 10 FLIGHT CONDITION

    Dohert, L.J. / Smart, M.K. / Mee, D.J. et al. | British Library Conference Proceedings | 2012

    DESIGN OF A MINIMUM TRIM HYPERSONIC AIRBREATHING ACCELERATOR VEHICLE

    Preller, D. / Smart, M.K. / American Institute of Aeronautics and Astronautics | 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

    CONTROL-ORIENTED 3D MODELING OF FLEXIBLE HYPERSONIC VEHICLES

    Su, E. / Luo, J. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2012

    CONCEPT STUDY OF AN ATMOSPHERIC REENTRY USING A WINGED UNMANNED SPACE VEHICLE

    Palumbo, R. / Morani, G. / De Stefano Fumo, M. et al. | British Library Conference Proceedings | 2012

    COMPARISON BETWEEN PROBE STAGNATION POINT HEAT FLUX MEASUREMENTS AND CORRELATION FORMULAS IN SCIROCCO PLASMA WIND TUNNEL TESTS

    Purpura, C. / Filippis, D. / Trifoni, E. 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

    CHEMILUMINESCENCE IMAGING IN A SUPERSONIC COMBUSTOR OPERATING IN RADICAL FARMING MODE

    Brieschenk, S. / Lorrain, P. / Capra, B.R. et al. | British Library Conference Proceedings | 2012

    CHECKOUT TESTING OF THE NEW BASIC PROCESS CONTROL SYSTEM AT THE AERODYNAMIC AND PROPULSION TEST UNIT

    Garrard, D. / Vaughn, D. / Milhoan, A. 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

    CALIBRATION OF THERMAL PAINTS FOR SURFACE TEMPERATURE MEASUREMENT OF HIFIRE-0 FLIGHT

    Choudhury, R. / Neely, A.J. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2012

    BRAZILIAN 14-X HYPERSONIC AEROSPACE VEHICLE PROJECT

    Toro, P.G.P. / Minucci, M.A.S. / Rolim, T.C. et al. | British Library Conference Proceedings | 2012

    BOUNDARY LAYER TRANSITION ON THE LEA HYPERSONIC VEHICLE FOREBODY

    Fedioun, I. / Orlik, E. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2012

    BLUNTNESS EFFECTS ON LIFT-TO-DRAG RATIO OF LEADING EDGES FOR HYPERSONIC WAVERIDER CONFIGURATIONS

    Santos, W.F.N. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2012

    A THERMAL ANALYSIS METHOD FOR FUEL-COOLED COMBUSTOR STRUCTURE BASED ON HEAT FLUX MEASUREMENT

    Lu, Y. / Li, L. / Fan, X. 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

    ASCENT TRAJECTORY OPTIMISATION FOR A SINGLE-STAGE-TO-ORBIT VEHICLE WITH HYBRID PROPULSION

    Pescetelli, F. / Minisci, E. / Maddock, C. et al. | British Library Conference Proceedings | 2012

    APPLICATION OF THE gamma -R e~0~tTRANSITION MODEL IN HIGH SPEED FLOWS

    You, Y. / Luedeke, H. / Eggers, T. et al. | British Library Conference Proceedings | 2012