Synonyme wurden verwendet für: Waves
Suche ohne Synonyme: keywords:(Mach Waves)

81–100 von 149 Ergebnissen
|

    Modeling of Thermodynamic Fluctuations in Canonical Shock–Turbulence Interaction

    Sethuraman, Yogesh Prasaad Madras / Sinha, Krishnendu | AIAA | 2020
    Schlagwörter: Shock Waves , Mach Numbers

    High-Order Accurate Numerical Method for Complex Flows

    Gross, A. / Fasel, H. F. | AIAA | 2008
    Schlagwörter: Mach Number , Tollmien Schlichting waves

    Relation Between Geometry and Wake Characteristics of a Supersonic Microramp

    Tambe, Sumit / Schrijer, Ferry / van Oudheusden, Bas | AIAA | 2021
    Schlagwörter: Shock Waves , Freestream Mach Number

    Use of Thermal Nonuniformity to Reduce Supersonic Jet Noise

    Daniel, Kyle A. / Mayo, David E. / Todd Lowe, K. et al. | AIAA | 2019
    Schlagwörter: Mach Waves

    Experimental Study of the Performance of a Rotating Detonation Engine with Nozzle

    Fotia, Matthew L. / Schauer, Fred / Kaemming, Tom et al. | AIAA | 2015
    Schlagwörter: Mach Number , Detonation Waves

    Prediction of Turbulent Jet Mixing Noise Reduction by Water Injection

    Kandula, Max | AIAA | 2008
    Schlagwörter: Mach Waves

    Experimental Study of Shock Oscillation over a Transonic Supercritical Profile

    Jacquin, L. / Molton, P. / Deck, S. et al. | AIAA | 2009
    Schlagwörter: Freestream Mach Number , Shock Waves

    Boundary-Layer Development Downstream of Normal Shock in Transonic Intakes at Incidence

    Coschignano, A. / Babinsky, H. | AIAA | 2019
    Schlagwörter: Shock Waves , Freestream Mach Number

    Influences of Inlet Geometry Modification on Scramjet Flow and Combustion Dynamics

    Liu, Qili / Baccarella, Damiano / Lee, Tonghun et al. | AIAA | 2017
    Schlagwörter: Shock Waves , Freestream Mach Number

    Nonlinear Aerodynamic and Aeroelastic Model Reduction Using a Discrete Empirical Interpolation Method

    Yao, W. / Marques, S. | AIAA | 2017
    Schlagwörter: Freestream Mach Number , Shock Waves

    Effects of Porous Walls on Hypersonic Boundary Layers over a Sharp Cone

    Stephen, Sharon O. / Michael, Vipin | AIAA | 2013
    Schlagwörter: Freestream Mach Number , Tollmien Schlichting waves

    Image-Based Analysis of Shock-Wave/Boundary-Layer Interaction Unsteadiness

    Combs, Christopher S. / Kreth, Phillip A. / Schmisseur, John D. et al. | AIAA | 2017
    Schlagwörter: Shock Waves , Mach Number

    Numerical Study on Wall Temperature Effects on Shock Wave/Turbulent Boundary-Layer Interaction

    Zhu, Xing-Kun / Yu, Chang-Ping / Tong, Fu-Lin et al. | AIAA | 2016
    Schlagwörter: Shock Waves , Freestream Mach Number

    Multi-Objective Aeroacoustic Design Exploration of Launch-Pad Flame Deflector Using Large-Eddy Simulation

    Tatsukawa, Tomoaki / Nonomura, Taku / Oyama, Akira et al. | AIAA | 2016
    Schlagwörter: Mach Waves

    Hypersonic Transitional Shock-Wave–Boundary-Layer Interaction on a Flat Plate

    Currao, Gaetano M. D. / Choudhury, Rishabh / Gai, Sudhir L. et al. | AIAA | 2019
    Schlagwörter: Shock Waves , Freestream Mach Number

    Vortex Generators for Corner Separation Caused by Shock-Wave/Boundary-Layer Interactions

    Koike, Shunsuke / Babinsky, Holger | AIAA | 2018
    Schlagwörter: Shock Waves , Mach Numbers

    Parametric Cycle Analysis of an Ideal Pulse Detonation Engine

    Roux, J. A. | AIAA | 2014
    Schlagwörter: Freestream Mach Number , Detonation Waves

    Skylon Aerospace Plane and Its Aerodynamics and Plumes

    Mehta, Unmeel / Aftosmis, Michael / Bowles, Jeffrey et al. | AIAA | 2016
    Schlagwörter: Freestream Mach Number , Shock Waves

    Stabilization of a Mach 5.92 Boundary Layer by Two-Dimensional Finite-Height Roughness

    Duan, Le / Wang, Xiaowen / Zhong, Xiaolin | AIAA | 2012
    Schlagwörter: Mach Waves

    Numerical Analysis of Ignition Overpressure Effect on H-IIB Launch Vehicle

    Tsutsumi, Seiji / Takaki, Ryoji / Hara, Toshiaki et al. | AIAA | 2014
    Schlagwörter: Shock Waves , Mach Number