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

101–120 von 188 Ergebnissen
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    Vortex Generators for Corner Separation Caused by Shock-Wave/Boundary-Layer Interactions

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

    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

    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

    Shape Optimization of Vortex Generators to Control Mack Mode Amplification

    Clark C Pederson / Meelan M Choudhari / Beckett Y Zhou et al. | NTRS | 2020
    Schlagwörter: Freestream Mach Number , Tollmien Schlichting waves

    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

    Design of Control-Assisted Transonic Pressure Recovery Profiles Using Vortex Generators

    Collazo Garcia, Armando R. / Ansell, Phillip J. | AIAA | 2021
    Schlagwörter: Freestream Mach Number , Tollmien Schlichting waves

    Comparison of Shock/Cooling-Film Interaction for Cooled and Isoenergetic Injection

    Marquardt, Pascal / Klaas, Michael / Schröder, Wolfgang | AIAA | 2020
    Schlagwörter: Freestream Mach Number , Shock Waves

    A Novel Reduced-Order Model for Predicting Compressible Cavity Flows

    Liu, Zhe / Ning, Fangli / Zhai, Qingbo et al. | AIAA | 2021
    Schlagwörter: Shock Waves , Mach Numbers

    Thermal Performance of Transonic Cooled Tips in a Turbine Cascade

    Zhou, Chao | AIAA | 2015
    Schlagwörter: Shock Waves , Mach Numbers

    Single-Camera Three-Dimensional Velocity Measurement of a Fin-Generated Shock-Wave/Boundary-Layer Interaction

    Jones, Cassandra / Bolton, Johnathan / Clifford, Christopher et al. | AIAA | 2020
    Schlagwörter: Shock Waves , Freestream Mach Number

    High-Speed Schlieren and Particle Image Velocimetry of the Exhaust Flow of a Pulse Detonation Combustor

    Haghdoost, Mohammad Rezay / Edgington-Mitchell, Daniel / Paschereit, Christian Oliver et al. | AIAA | 2020
    Schlagwörter: Prandtl Meyer Expansion Waves , Mach Numbers

    Buzz Cycle Description in an Axisymmetric Mixed-Compression Air Intake

    Soltani, Mohammad Reza / Sepahi-Younsi, Javad | AIAA | 2015
    Schlagwörter: Freestream Mach Number , Shock Waves

    Feedback Mechanism in Supersonic Laminar Cavity Flows

    Li, Weipeng / Nonomura, Taku / Oyama, Akira et al. | AIAA | 2012
    Schlagwörter: Mach Waves

    A Near-Field Approach to the Sonic Boom Problem

    F. A. Woodward | NTIS | 1967
    Schlagwörter: Shock waves , Mach cones , Mach number

    Investigation of Shear Layer Growth Influenced by Shock Waves in a Scramjet

    Cao, Donggang / He, Guoqiang / Qin, Fei et al. | AIAA | 2016
    Schlagwörter: Shock Waves , Mach Number

    Gas-Kinetic Harmonic Balance Method for Unsteady Supersonic/Hypersonic Flows with Oscillating Motions

    Zhou, Di / Lu, Zhiliang / Guo, Tongqing et al. | AIAA | 2019
    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

    High-Fidelity Simulations of Pressure-Gain Combustion Devices Based on Detonations

    Kailasanath, K. / Schwer, D. A. | AIAA | 2016
    Schlagwörter: Detonation Waves , Mach Numbers

    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