Synonyms were used for: HYPERSCHALL
Search without synonyms: keywords:(HYPERSCHALL)

61–80 of 4,251 hits
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    Hydrogen for Hypersonic Civil Transportation

    Mehta, Unmeel | NTRS | 2017
    Keywords: Hypersonic

    Survey of planetary entry guidance algorithms

    D׳Souza, Sarah N. / Sarigul-Klijn, Nesrin | Elsevier | 2014
    Keywords: Hypersonic

    Active flow control by a novel combinational active thermal protection for hypersonic vehicles

    Huang, Jie / Yao, Wei-Xing | Elsevier | 2020
    Keywords: Hypersonic

    BiGlobal stability analysis of the wake behind an isolated roughness element in hypersonic flow

    Free access
    Montero, Iván Padilla / Pinna, Fabio | SAGE Publications | 2020
    Keywords: hypersonic

    Numerical simulation of hypersonic flow over highly blunted cones with spike

    Gerdroodbary, M. Barzegar / Hosseinalipour, S.M. | Elsevier | 2010
    Keywords: Hypersonic flow

    FLEET and PLIF Velocimetry Within A Mach 10 Hypersonic Air Flow

    Neil S Rodrigues / Olivia K Tyrrell / Elizabeth F Rieken et al. | NTRS
    Keywords: Hypersonic

    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
    Keywords: Hypersonic systems

    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
    Keywords: Hypersonic systems

    WATER INJECTION PRE-COMPRESSOR COOLING ASSIST SPACE ACCESS

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

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

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

    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
    Keywords: Hypersonic systems

    A NEW DYNAMIC LES/RANS HYBRID METHOD

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

    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
    Keywords: Hypersonic systems

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

    Lee, S. / Watanabe, J. / Kouchi, T. et al. | British Library Conference Proceedings | 2012
    Keywords: Hypersonic systems

    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
    Keywords: Hypersonic systems

    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
    Keywords: Hypersonic systems

    VALIDATION OF PIV MEASUREMENTS USING SUPERSONIC TURBULENT BOUNDARY LAYER

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

    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
    Keywords: Hypersonic systems

    Simulation of Hypersonic-Shock-Wave–Laminar-Boundary-Layer Interaction over Blunt Fin

    Mortazavi, Mahsa / Knight, Doyle | AIAA | 2019
    Keywords: Hypersonic Shock Waves , Hypersonic Flows , Hypersonic Aircraft

    Effect of Leading-Edge Bluntness on Shockwave–Boundary-Layer Interaction in a Scramjet Intake

    Vamsi Krishna, Talluri / Sreekumar, Jithin / Ibrahim Sugarno, Mohammed et al. | AIAA | 2024
    Keywords: Hypersonic Aerodynamics , Hypersonic Inlets , Hypersonic Shock