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

121–140 von 149 Ergebnissen
|

    Effect of Nozzle–Plate Distance on Acoustic Phenomena from Supersonic Impinging Jet

    Akamine, Masahito / Okamoto, Koji / Gee, Kent L. et al. | AIAA | 2018
    Schlagwörter: Mach Waves

    Aerothermal Performance of Different Tips in Transonic Turbine Cascade with End-Wall Motion

    Zhou, Chao | AIAA | 2014
    Schlagwörter: Shock Waves , Mach Numbers

    Aeroacoustics of a Planar Multistream Supersonic Nozzle with Aft Deck and Sidewalls

    Tinney, Charles E. / Panickar, Praveen / Vogel, Patrick | AIAA | 2018
    Schlagwörter: Mach Waves

    Performance and Energy Expenditure of Coflow Jet Airfoil with Variation of Mach Number

    Lefebvre, A. / Dano, B. / Bartow, W. B. et al. | AIAA | 2016
    Schlagwörter: Freestream Mach Number , Shock Waves

    Characterizing Streamwise Development of Surface Roughness Effects on a Supersonic Boundary Layer

    Kocher, Brian D. / Kreth, Phillip A. / Schmisseur, John D. et al. | AIAA | 2022
    Schlagwörter: Prandtl Meyer Expansion Waves , Freestream Mach Number

    Effect of Microramps on Separated Swept Shock Wave–Boundary-Layer Interactions

    Martis, Roschelle R. / Misra, Ajay / Singh, Amarjit | AIAA | 2014
    Schlagwörter: Shock Waves , Freestream Mach Number

    Characterization of Turbulent Supersonic Flow over a Backward-Facing Step

    Soni, R. K. / Arya, N. / De, Ashoke | AIAA | 2017
    Schlagwörter: Shock Waves , Mach Number

    Modal Decomposition Analysis of Three-Dimensional Transonic Buffet Phenomenon on a Swept Wing

    Ohmichi, Yuya / Ishida, Takashi / Hashimoto, Atsushi | AIAA | 2018
    Schlagwörter: Shock Waves , Freestream Mach Number

    Wave-Packet Representation of Shock-Cell Noise for a Single Round Jet

    Suzuki, Takao | AIAA | 2016
    Schlagwörter: Shock Waves , Acoustic Mach Number

    Modification of Ninth-Order Weighted Essentially Nonoscillatory Scheme for Mixed Subsonic/Supersonic Flow

    Gross, A. / Fasel, H. F. | AIAA | 2010
    Schlagwörter: Freestream Mach Number , Tollmien Schlichting waves

    Pressure-Gain Combustion Using Shock–Flame Interaction

    Lutoschkin, E. / Rose, M. G. / Staudacher, S. | AIAA | 2013
    Schlagwörter: Detonation Waves , Mach Numbers

    Influence of External Flow on Plume Physics of Clustered Linear Aerospike Nozzles

    Takahashi, Hidemi / Tomioka, Sadatake / Sakuranaka, Noboru et al. | AIAA | 2014
    Schlagwörter: Mach Waves

    Simulations of Cellular Detonation Interaction with Turbulent Flows

    Jin, Tai / Luo, Kun / Dai, Qi et al. | AIAA | 2015
    Schlagwörter: Detonation Waves , Freestream Mach Number

    Global Sensitivity Analysis and Uncertainty Quantification for a Hypersonic Shock Interaction Flow

    Burt, Jonathan M. / Josyula, Eswar | AIAA | 2015
    Schlagwörter: Hypersonic Shock Waves , Freestream Mach Number

    Response of a Hypersonic Boundary Layer to Wall Blowing-Suction

    Wang, Xiaowen / Zhong, Xiaolin / Ma, Yanbao | AIAA | 2011
    Schlagwörter: Tollmien Schlichting waves , Freestream Mach Number

    Investigation of Surface Curvature Effects on Unseparated Fin Shock-Wave/Boundary-Layer Interactions

    Pickles, Joshua D. / Narayanaswamy, Venkateswaran | AIAA | 2019
    Schlagwörter: Shock Waves , Freestream Mach Number

    Scaling of Upstream Influence Line Induced by Shock Sweeping Concave Half-Cylinder

    Huang, Qi / Hong, Yuting / Li, Zhufei | AIAA | 2024
    Schlagwörter: Shock Waves , Freestream Mach Number

    Aerodynamics of a Supersonic Projectile in Proximity to a Solid Surface

    Doig, Graham / Barber, Tracie J. / Leonardi, Eddie et al. | AIAA | 2010
    Schlagwörter: Mach Waves

    Studies of Inlet Distortion in a Direct-Connect Axisymmetric Scramjet Isolator

    Tam, Chung-Jen / Hsu, Kuang-Yu / Hagenmaier, Mark et al. | AIAA | 2013
    Schlagwörter: Strong Oblique Shock Waves , Mach Numbers

    Experimental and Numerical Investigation of a Supersonic Convergent-Divergent Nozzle

    Burak, Markus O. / Eriksson, Lars-Erik / Munday, David et al. | AIAA | 2012
    Schlagwörter: Mach Numbers , Prandtl Meyer Expansion Waves