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

61–80 von 191 Ergebnissen
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    Mixing Characteristics of Active Microjet-Based Actuators in a Supersonic Backward-Facing-Step Flow

    Ahmed, Kareem A. / Ali, Mohd Y. / Alvi, Farrukh S. | AIAA | 2014
    Schlagwörter: Mach Waves

    Summary of Propagation Cases of the Third AIAA Sonic Boom Prediction Workshop

    Rallabhandi, Sriram K. / Loubeau, Alexandra | AIAA | 2021
    Schlagwörter: Evanescent Waves , Mach Number

    Microramp Control of Supersonic Oblique Shock-Wave/Boundary-Layer Interactions

    Babinsky, H. / Li, Y. / Ford, C. W. Pitt | AIAA | 2009
    Schlagwörter: Shock Waves , Freestream Mach Number

    Detonation Stabilization in Supersonic Flow: Effects of Suction Boundaries

    Cai, Xiaodong / Deiterding, Ralf / Liang, Jianhan et al. | AIAA | 2019
    Schlagwörter: Mach Reflection , Detonation Waves

    Performance Sensitivities of Rotating Detonation Engines Installed onto Waverider Forebodies

    Mizener, Andrew R. / Lu, Frank K. / Rodi, Patrick E. | AIAA | 2019
    Schlagwörter: Freestream Mach Number , Detonation Waves

    Investigating Unsteady Dynamics of Cylinder-Induced Shock-Wave/Transitional Boundary-Layer Interactions

    Combs, Christopher S. / Lash, E. Lara / Kreth, Phillip A. et al. | AIAA | 2018
    Schlagwörter: Shock Waves , Freestream Mach Number

    Direct Numerical Simulation of a Reflected-Shock-Wave/Turbulent-Boundary-Layer Interaction

    Priebe, S. / Wu, M. / Martín, M. P. | AIAA | 2009
    Schlagwörter: Shock Waves , Freestream Mach Number

    Modeled Boltzmann Equation and Its Application to Shock-Capturing Simulation

    So, R. M. C. / Leung, R. C. K. / Fu, S. C. | AIAA | 2008
    Schlagwörter: Mach Numbers , Planar Waves

    Characterization of Unsteadiness in an Overexpanded Planar Nozzle

    Martelli, E. / Ciottoli, P. P. / Saccoccio, L. et al. | AIAA | 2018
    Schlagwörter: Shock Waves , Mach Number

    Effects of Feeding Pressures on the Flowfield Structures of Supersonic Film Cooling

    Song, Changqing / Shen, Chibing | AIAA | 2017
    Schlagwörter: Shock Waves , Mach Number

    Effects of Divergence Inlet on Kerosene/Air Rotating Detonation Engines

    Wang, Fang / Weng, Chunsheng | AIAA | 2022
    Schlagwörter: Mach Numbers , Detonation Waves

    Deriving Features of Reacting Hypersonic Flow from Gradients at a Curved Shock

    Hornung, H. G. | AIAA | 2010
    Schlagwörter: Detonation Waves , Freestream Mach Number

    Local Flow Conditions for Propulsion Experiments on the NASA F-15B Propulsion Flight Test Fixture

    M. J. Vachon / T. R. Moes / S. Corda | NTIS | 2005
    Schlagwörter: Mach number , Shock waves

    Eddy Convection in Developing Heated Supersonic Jets

    Ecker, Tobias / Lowe, K. Todd / Ng, Wing F. | AIAA | 2015
    Schlagwörter: Mach Waves

    Transition Between Different Initiation Structures of Wedge-Induced Oblique Detonations

    Zhang, Yining / Yang, Pengfei / Teng, Honghui et al. | AIAA | 2018
    Schlagwörter: Detonation Waves , Mach Number

    Experimental Investigation of Isoenergetic Film-Cooling Flows with Shock Interaction

    Marquardt, Pascal / Klaas, Michael / Schröder, Wolfgang | AIAA | 2019
    Schlagwörter: Freestream Mach Number , Shock Waves

    Wall Temperature and Suction Control of Linear Modes in Compressible Corner Flow

    Staudenmeyer, J. / Schnoebel, N. / Rist, U. | AIAA | 2019
    Schlagwörter: Mach Numbers , Tollmien Schlichting waves

    Modeling of Thermodynamic Fluctuations in Canonical Shock–Turbulence Interaction

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

    Front Cellular Structure and Thrust Performance on Hydrogen–Oxygen Rotating Detonation Engine

    Tsuboi, Nobuyuki / Eto, Seiichiro / Hayashi, A. Koichi et al. | AIAA | 2016
    Schlagwörter: Mach Number , Detonation Waves

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

    Mortazavi, Mahsa / Knight, Doyle | AIAA | 2019
    Schlagwörter: Hypersonic Shock Waves , Freestream Mach Number