Synonyme wurden verwendet für: BOUNDARY LAYER NOZZLES
Suche ohne Synonyme: keywords:(BOUNDARY LAYER - NOZZLES)

1–20 von 109 Ergebnissen
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    Numerical study of ways to prevent side loads in an over–expanded rocket nozzles during the launch stage

    Ivanov, I.E. / Kryukov, I.A. | Elsevier | 2019
    Schlagwörter: Boundary layer flow in nozzles

    Supersonic flow separation with application to rocket engine nozzles

    Östlund, J. / Muhammad-Klingmann, B. | Tema Archiv | 2005
    Schlagwörter: Düse , Grenzschicht

    Navier–Stokes Simulation of Graphite Nozzle Erosion at Different Pressure Conditions

    Bianchi, Daniele | Online Contents | 2015
    Schlagwörter: Nozzles , Boundary layer

    Development of a Short-Duration Rocket Nozzle Flow Simulation Facility

    Yahiaoui, G | Online Contents | 2015
    Schlagwörter: Nozzles , Boundary layer

    Extending the 15in x 15in Arizona Supersonic Wind Tunnel to Transonic Conditions

    J. Little | NTIS | 2023
    Schlagwörter: Boundary layer , Boundary layer transition , Subsonic nozzles

    Wake dynamics and exhaust distribution behind cruising aircraft

    Gerz, T. / Ehret, T. | Tema Archiv | 1996
    Schlagwörter: Düse , Grenzschicht

    On the Application of the Abel Transformation in Statistically Axisymmetric Turbulent Flows

    Schmidt, Bryan E. / Page, Wayne E. / Sutton, Jeffrey A. | AIAA | 2022
    Schlagwörter: Circular Nozzles , Turbulent Boundary Layer

    Suction and Oscillatory Blowing Actuator Modeling and Validation

    Arwatz, Gilad / Fono, Ilan / Seifert, Avi | AIAA | 2008
    Schlagwörter: Incompressible Boundary Layer , Inlet Nozzles

    Nozzle Geometry Effects on Corner Boundary Layers in Supersonic Wind Tunnels

    Sabnis, Kshitij / Babinsky, Holger | AIAA | 2019
    Schlagwörter: Boundary Layer Separation , Contoured Nozzles

    Corrugated Tabs for Supersonic Jet Control

    Phanindra, B. Chiranjeevi / Rathakrishnan, E. | AIAA | 2010
    Schlagwörter: Convergent Divergent Nozzles , Boundary Layer Thickness

    Optimization of a Rocket Nozzle Side Load Reduction Device

    Stark, R. / Génin, C. | AIAA | 2016
    Schlagwörter: Boundary Layer Transition , Convergent Divergent Nozzles

    Hybrid Reynolds-Averaged/Large-Eddy Simulations of a Coaxial Supersonic Freejet Experiment

    Baurle, R. A. / Edwards, J. R. | AIAA | 2010
    Schlagwörter: Boundary Layer Thickness , Coaxial Nozzles

    Production of High-Mach-Number Scramjet Flow Conditions in an Expansion Tube

    Gildfind, David E. / Morgan, Richard G. / Jacobs, Peter A. et al. | AIAA | 2013
    Schlagwörter: Contoured Nozzles , Boundary Layer Thickness

    Radiative Heat Transfer in Solid Rocket Nozzles

    Cross, Peter G. | AIAA | 2019
    Schlagwörter: Thermal Boundary Layer , Axisymmetric Nozzles

    Active Control of Dual-Bell Nozzle Operation Mode Transition by Film Cooling and Mixture Ratio Variation

    Schneider, Dirk / Stark, Ralf / Génin, Chloé et al. | AIAA | 2019
    Schlagwörter: Convergent Divergent Nozzles , Boundary Layer Thickness

    Experimental Flowfield Analyses of Installed Subsonic Jet–Pylon Interaction

    Proença, Anderson R. / Lawrence, Jack L. T. | AIAA | 2021
    Schlagwörter: Axisymmetric Nozzles , Boundary Layer Thickness

    Aerodynamic Design of Nozzles with Uniform Outflow for Hypervelocity Ground-Test Facilities

    Chan, Wilson Y. K. / Jacobs, Peter A. / Smart, Michael K. et al. | AIAA | 2018
    Schlagwörter: Axisymmetric Nozzles , Boundary Layer Transition

    Modeling Swirl Evolution Inside Annular Nozzles Under Compressible Effect

    Gong, Young Keon / Do, Hyungrok / Lee, Gilbong et al. | AIAA | 2022
    Schlagwörter: Circular Nozzles , Boundary Layer

    Timescale-Based Frozen Nonadiabatic Flamelet Combustion Modeling for Rocket Engine Thrust Chambers

    Rahn, Daniel / Haidn, Oskar / Riedmann, Hendrik | AIAA | 2021
    Schlagwörter: Divergent Nozzles , Boundary Layer Thickness

    New Strategies for Mitigating the Gray Area in Delayed-Detached Eddy Simulation Models

    Pont-Vílchez, Arnau / Duben, Alexey / Gorobets, Andrey et al. | AIAA | 2021
    Schlagwörter: Boundary Layer Thickness , Conical Nozzles