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

1–50 von 181 Ergebnissen
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    A Coupled Inviscid–Viscous Airfoil Analysis Solver, Revisited

    Fidkowski, Krzysztof J. | AIAA | 2021
    Schlagwörter: Tollmien Schlichting waves , Freestream Mach Number

    Acoustic Propagation Using Computational Fluid Dynamics

    J. D. Baeder / W. J. McCroskey / G. R. inivasan | NTIS | 1986
    Schlagwörter: Mach number , Shock waves

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

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

    Aeroacoustics of Three-Stream High-Speed Jets from Coaxial and Asymmetric Nozzles

    Papamoschou, Dimitri / Johnson, Andrew D. / Phong, Vincent | AIAA | 2014
    Schlagwörter: Mach Numbers , Mach Waves

    Aerodynamic Phenomena in Supersonic Flow

    Torenbeek, Egbert | Wiley | 2020
    Schlagwörter: shock waves , normal shock waves , mach waves , streamlines waves

    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

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

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

    A method for predicting Mach stem height in steady flows

    Choe, Song-Guk | SAGE Publications | 2022
    Schlagwörter: Mach stem , shock waves

    Analytical, Numerical, and Experimental Investigations of Oblique-Shock-Wave Reflections in Pure and Dusty Gases

    I. I. Glass | NTIS | 1987
    Schlagwörter: Shock waves , TDMR(Terminal Double Mach Reflection)

    A Near-Field Approach to the Sonic Boom Problem

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

    An Estimate of Turbulent Velocities in the Ocean

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

    Antisymmetric Oscillation Modes in Rectangular Screeching Jets

    Gojon, Romain / Gutmark, Ephraim / Mihaescu, Mihai | AIAA | 2019
    Schlagwörter: Mach Number , Mach Waves

    A Plane Hypersonic Gas Stream

    M. I. Folle | NTIS | 1970
    Schlagwörter: Mach number , Shock waves

    A Wind Tunnel Flight Correlation of APOLLO 16 Sonic Boom

    F. Garcia / R. M. Hicks / J. P. Mendoza | NTIS | 1973
    Schlagwörter: Mach number , Shock waves

    Back-Pressure Effects on the Hypersonic Inlet-Isolator Pseudoshock Motions

    Su, Wei-Yi / Zhang, Kun-Yuan | AIAA | 2013
    Schlagwörter: Shock Waves , Freestream Mach Number

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

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

    Buzz Cycle Description in an Axisymmetric Mixed-Compression Air Intake

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

    Causal Analysis of Flowfields Using Clustering Entropy

    Omata, Noriyasu / Tsutsumi, Seiji | AIAA | 2020
    Schlagwörter: Mach Waves

    Characterization of Turbulent Supersonic Flow over a Backward-Facing Step

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

    Characterization of Unsteadiness in an Overexpanded Planar Nozzle

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

    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

    Coherence Analysis of the Noise from a Simulated Highly Heated Laboratory-Scale Jet

    Leete, Kevin M. / Gee, Kent L. / Liu, Junhui et al. | AIAA | 2020
    Schlagwörter: Mach Waves , Mach Number

    Collision-Free Shocks in the Laboratory and Space

    NTIS | 1969
    Schlagwörter: Bow waves , Magnetohydrodynamic waves , Shock waves , Mach number , Plasma 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

    Confined Detonations and Pulse Detonation Engines

    G. D. Roy / S. M. Frolov / R. J. Santoro et al. | NTIS | 2003
    Schlagwörter: Mach number , Detonation waves

    Control of Fin Shock Induced Flow Separation Using Vortex Generators

    Pickles, Joshua D. / Narayanaswamy, Venkateswaran | AIAA | 2020
    Schlagwörter: Shock Waves , Mach Numbers

    Correlation of Flowfield and Acoustic field Measurements in High-Speed Jets

    Veltin, Jérémy / Day, Benjamin J. / McLaughlin, Dennis K. | AIAA | 2011
    Schlagwörter: Mach Waves , Acoustic Mach Number

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

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

    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

    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

    Detonation Initiation in a Tube via Imploding Toroidal Shock Waves

    Jackson, S. I. / Shepherd, J. E. | AIAA | 2008
    Schlagwörter: Detonation Waves , Mach Reflection , Planar Waves

    Detonation Simulations in Supersonic Combustible Mixtures with Nonuniform Species

    Cai, Xiaodong / Liang, Jianhan / Deiterding, Ralf et al. | AIAA | 2016
    Schlagwörter: Mach Reflection , Detonation Waves , Mach Numbers

    Detonation Stabilization in Supersonic Flow: Effects of Suction Boundaries

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

    Development of a high temperature rotary actuator for aircraft hydraulic systems

    Ausdal, R.K.van | Tema Archiv | 1978
    Schlagwörter: WELLE (MASCHINENELEMENT) , MACH-ZAHL

    Die experimentelle Bestimmung der Stofftemperatur hinter starken Stosswellen in Argon bei Mach-Zahlen von 8 bis 30

    Ilmetov, A. / Titov, V. | Tema Archiv | 1978
    Schlagwörter: MACH-ZAHL , WELLE

    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

    Direct Numerical Simulation of Hypersonic Transition Delay over Carbon/Carbon Ultrasonically Absorptive Coatings

    C. Scalo | NTIS | 2019
    Schlagwörter: Mach zehnder interferometers , Sound waves , Second-mode waves

    Direct Visualization of Shock Waves in Supersonic Space Shuttle Flight

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

    Drag Reduction by Boundary-Layer Combustion: Effects of Flow Disturbances from Rectangular-to-Elliptical-Shape-Transition Inlets

    Chan, Wilson Y. K. / Mee, David J. / Smart, Michael K. et al. | AIAA | 2015
    Schlagwörter: Freestream Mach Number , Shock Waves

    Eddy Convection in Developing Heated Supersonic Jets

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

    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

    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

    Effects of Divergence Inlet on Kerosene/Air Rotating Detonation Engines

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

    Effects of Jet Temperature on Broadband Shock-Associated Noise

    Kuo, Ching-Wen / McLaughlin, Dennis K. / Morris, Philip J. et al. | AIAA | 2014
    Schlagwörter: Acoustic Mach Number , Mach 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

    Effects of Strong Wall Cooling on Supersonic and Hypersonic Shock/Boundary-Layer Interactions

    J. Larsson / T. Zaki | NTIS | 2019
    Schlagwörter: Mach number , Shock waves

    Evaluation of Uncertainties of Pressure Gain Measurements in Rotating Detonation Combustor

    Feleo, Alexander D. / Gamba, Mirko | AIAA | 2023
    Schlagwörter: Choking Mach Number , Detonation Waves