21–40 von 160 Ergebnissen
|

    A NEW METHOD FOR CALIBRATING FLOW FIELD OF HYPERSONIC NOZZLE

    Tiejin, W. / Yongtang, S. / Xuejun, Z. et al. | British Library Conference Proceedings | 2012

    SIMULATION OF HIGH MACH NUMBER SCRAMJET FLOW CONDITIONS USING THE X2 EXPANSION TUBE

    Gildfinder, D.E. / Morgan, R.G. / McGilvray, M. et al. | British Library Conference Proceedings | 2012

    ANALYSIS AND CORRELATION OF FLAME STABILITY LIMITS IN SUPERSONIC FLOW WITH CAVITY FLAMEHOLDER

    Le, J. / Yang, S. / Wang, X. et al. | British Library Conference Proceedings | 2012

    WATER INJECTION PRE-COMPRESSOR COOLING ASSIST SPACE ACCESS

    Mehta, U. / Bowles, J. / Melton, J. et al. | British Library Conference Proceedings | 2012

    THE THEORETICAL STUDY OF THE AERO-THERMODYNAMICS CHARACTERISTICS FOR SCRAMJET COMBUSTOR

    Lin, X. / Qina, L. / Shengwei, X. et al. | British Library Conference Proceedings | 2012

    RAPID THREE-DIMENSIONAL CONSTRAINED TRAJECTORY GENERATION FOR NEAR SPACE HYPERSONIC VEHICLES

    Dong, C. / Chao, T. / Wang, S.-Y. et al. | British Library Conference Proceedings | 2012

    A NEW DYNAMIC LES/RANS HYBRID METHOD

    Gao, R. / Xu, J. / Yan, C. et al. | British Library Conference Proceedings | 2012

    THERMAL PROTECTION AND HYDROGEN PRODUCTION ON BOARD OF THE HYPERSONIC VEHICLE

    Kuranov, A.L. / Korabelnikov, A.V. / Mikhailov, A.M. et al. | British Library Conference Proceedings | 2012

    LARGE-EDDY SIMULATION OF PSEUDO-SHOCK WAVE IN A SQUARE DUCT

    Lee, S. / Watanabe, J. / Kouchi, T. 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

    MULTI-OBJECTIVE OPTIMIZATION OF HYPERSONIC VEHICLES UNDER ASYMMETRIC BOUNDARY-LAYER CONDITIONS

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

    VALIDATION OF PIV MEASUREMENTS USING SUPERSONIC TURBULENT BOUNDARY LAYER

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

    TOWARDS ROBUST AERO-THERMODYNAMIC PREDICTIONS FOR RE-USABLE SINGLE-STAGE TO ORBIT VEHICLES

    Wuilbercq, R. / Ahmad, A. / Scanlon, T. 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

    EXPERIMENTAL INVESTIGATION ON COUPLING CHARACTERISTICS OF CAVITY FLAMEHOLDER AND STRUT JET

    Hongbin, G. / Lihong, C. / Dan, W. 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

    SHOCK TUBE TESTING OF THE TRANSPIRATION-COOLED HEAT SHIELD EXPERIMENT AKTIV

    Bohrk, H. / Wartemann, V. / Eggers, T. et al. | British Library Conference Proceedings | 2012

    NUMERICAL STUDY OF IGNITION AND COMBUSTION OF PARTIALLY CRACKED KEROSENE IN A MACH 2.5 SUPERSONIC MODEL COMBUSTOR

    Zhong, F. / Chen, L. / Chang, X. et al. | British Library Conference Proceedings | 2012

    TURBULENT FLOW SIMULATIONS OF A MIXTURE OF PERFECT GASES

    Noureldin, K.A. / Windisch, C. / Reinartz, B. et al. | British Library Conference Proceedings | 2012

    DISINTEGRATION REGIMES NEAR THE CRITICAL POINT

    Lamanna, G. / Oldenhof, E. / Baab, S. et al. | British Library Conference Proceedings | 2012