21–40 von 2,267 Ergebnissen
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    Visualization of Hypersonic Boundary-Layer Transition on a Slender Cone (Invited)

    Laurence, Stuart J. / Wagner, Alexander / Ozawa, Hiroshi et al. | AIAA | 2014
    Verlag: The American Institute of Aeronautics and Astronautics

    Viscous Performance Map of a Blunt Streamline-Traced Busemann Inlet

    O'Brien, Timothy | AIAA | 2011
    Verlag: The American Institute of Aeronautics and Astronautics

    Viscous-Optimized Length-Constrained Axisymmetric Geometries for Streamline-Tracing

    O'Brien, Timothy | AIAA | 2008
    Verlag: The American Institute of Aeronautics and Astronautics

    Viscous drag reduction in a scramjet combustor with film cooling

    Rowan, S. / Paull, A. | AIAA | 2001
    Verlag: The American Institute of Aeronautics and Astronautics

    Viscous Drag Reduction in a Mach 12 Scramjet Engine

    Rowan, Scott / Takahashi, Masahiro / Sunami, Tetsuji et al. | AIAA | 2005
    Verlag: The American Institute of Aeronautics and Astronautics

    Virtual Experiment for Optimization of Fuel Distribution in a Scramjet Engine

    Sato, Shigeru / Fukui, Masaaki / Watanabe, Takahiro et al. | AIAA | 2015
    Verlag: The American Institute of Aeronautics and Astronautics

    Velocity Profile Modification in High-Speed Flows

    Barkmeyer, Daniel / Lewis, Mark | AIAA | 2003
    Verlag: The American Institute of Aeronautics and Astronautics

    Velocity measurement in a dual-mode supersonic combustor using particle image velocimetry

    Goyne, C. / McDaniel, J. / Krauss, R. et al. | AIAA | 2001
    Verlag: The American Institute of Aeronautics and Astronautics

    Velocity Field in Secondary Combustor of Ejector-Jet

    Nojima, Kiyoshi / Kouchi, Toshinori / Masuya, Goro et al. | AIAA | 2012
    Verlag: The American Institute of Aeronautics and Astronautics

    VeLChYD - Very Low Cost Hypersonic Demonstrator for a Complete Orbital Reentry Mission

    Chiesa, Sergio / Corpino, Sabrina / Plucinski, Krzysztof et al. | AIAA | 2005
    Verlag: The American Institute of Aeronautics and Astronautics

    Vehicle Systems

    Bowles, David | AIAA | 2003
    Verlag: The American Institute of Aeronautics and Astronautics

    Vehicle evaluations for tether-assisted launch to orbit

    Martin, J. / Hollowell, S. | AIAA | 2001
    Verlag: The American Institute of Aeronautics and Astronautics

    Vehicle concepts for an ejector ramjet combined cycle engine

    Lentsch, A. / Taguchi, H. / Shepperd, R. et al. | AIAA | 2001
    Verlag: The American Institute of Aeronautics and Astronautics

    Validity of an Assumed PDF Combustion Model For SCRAMJET Applications

    Foerster, Henrik / Sattelmayer, Thomas | AIAA | 2008
    Verlag: The American Institute of Aeronautics and Astronautics

    Validation of Tools to Accelerate High-Speed CFD Simulations Using OpenFOAM

    Espinoza, Daniel E. / Scanlon, Thomas J / Brown, Richard E. | AIAA | 2015
    Verlag: The American Institute of Aeronautics and Astronautics

    Validation of the IXV Mission Analysis and Flight Mechanics Design

    Haya-Ramos, Rodrigo / Bonetti, Davide / Serna, Jorge et al. | AIAA | 2012
    Verlag: The American Institute of Aeronautics and Astronautics

    Validation of PIV measurements using Supersonic Turbulent Boundary Layer

    Yumiyama, M. / Sakaue, S. / Arai, T. | AIAA | 2012
    Verlag: The American Institute of Aeronautics and Astronautics

    Validation of global aeropropulsive characteristics of integrated configurations

    Chalot, Frederic / Rostand, Philippe / Perrier, Pierre et al. | AIAA | 1998
    Verlag: The American Institute of Aeronautics and Astronautics

    Validation of a Novel OpenFOAM Solver using a Supersonic, Non-reacting Channel Flow

    Droeske, Nils / Makowka, Konrad / Nizenkov, Paul et al. | AIAA | 2014
    Verlag: The American Institute of Aeronautics and Astronautics

    Validation of a Leak-free C/SiC Heat Exchanger Technology

    Bouquet, Clement | AIAA | 2003
    Verlag: The American Institute of Aeronautics and Astronautics