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

101–150 von 189 Ergebnissen
|

    Parametric Cycle Analysis of an Ideal Pulse Detonation Engine

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

    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

    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

    Skylon Aerospace Plane and Its Aerodynamics and Plumes

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

    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

    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

    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

    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

    Toward a Comprehensive Model of Jet Noise Using an Acoustic Analogy

    Miller, Steven A. E. | AIAA | 2014
    Schlagwörter: Mach Waves

    Buzz Cycle Description in an Axisymmetric Mixed-Compression Air Intake

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

    A Near-Field Approach to the Sonic Boom Problem

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

    Feedback Mechanism in Supersonic Laminar Cavity Flows

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

    Design of Low-Speed Slotted, Natural-Laminar-Flow Airfoil Reproducing Transonic Behaviors

    Coder, James G. | AIAA | 2020
    Schlagwörter: Drag Divergence Mach Number , Tollmien Schlichting waves

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

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

    Thermal Performance of Transonic Cooled Tips in a Turbine Cascade

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

    Film Cooling in Laminar and Turbulent Supersonic Flows

    Hombsch, M. / Olivier, H. | AIAA | 2013
    Schlagwörter: Mach Waves

    Experimental Study of Boundary-Layer Response to Laser-Generated Disturbances at Mach 6

    Heitmann, Dirk / Radespiel, Rolf / Knauss, Helmut | AIAA | 2013
    Schlagwörter: Freestream Mach Number , Tollmien Schlichting waves

    Numerical Investigation of Transitional Shock-Wave/Boundary-Layer Interaction in Supersonic Regime

    Quadros, Russell / Bernardini, Matteo | AIAA | 2018
    Schlagwörter: Shock Waves , Freestream 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

    Simulation of Laser-Induced Plasma Ignition in a Hypersonic Crossflow

    Gibbons, Nicholas / Gehre, Rolf / Brieschenk, Stefan et al. | AIAA | 2018
    Schlagwörter: Freestream Mach Number , Detonation Waves

    Shock-Induced Separation and Control in a 4.32-Aspect-Ratio Test Section

    Warning, Sally / Lambert, Scott / McQuilling, Mark et al. | AIAA | 2024
    Schlagwörter: Freestream Mach Number , Shock Waves

    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

    Direct Visualization of Shock Waves in Supersonic Space Shuttle Flight

    J. M. OFarrell / T. J. Rieckhoff | NTIS | 2011
    Schlagwörter: Shock waves , Mach number

    Wedge-Induced Oblique Detonations with Small Heat Release

    Domínguez-González, Alba / Martínez-Ruiz, Daniel / Scotzniovsky, Luca et al. | AIAA | 2021
    Schlagwörter: Freestream Mach Number , Detonation Waves

    Numerical Error in the k - ε Turbulence Model Applied to Eddy-Viscous Shock Waves

    Sinha, Krishnendu / Singh, Rachit S. | AIAA | 2016
    Schlagwörter: Shock Waves , Mach Numbers

    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

    Shock-Wave Patterns on a Cranked-Wing Configuration

    R. I. Sammonds | NTIS | 1960
    Schlagwörter: Shock waves , Bow waves , 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

    An Estimate of Turbulent Velocities in the Ocean

    T. E. Pochapsky | NTIS | 1959
    Schlagwörter: Ocean waves , Mach number

    Propagation from moving sources in flows

    Morfey, C.L. | Tema Archiv | 1979
    Schlagwörter: AKUSTISCHE WELLE , MACH-ZAHL

    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

    Determination of Sun Angles for Observations of Shock Waves on a Transport Aircraft

    D. F. Fisher / E. A. Haering / G. K. Noffz et al. | NTIS | 1998
    Schlagwörter: Mach number , Shock waves

    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