1–20 von 76 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

    Validation study of numerical simulations by comparison to measurements in piston-driven shock-tunnels

    Mundt, Christian / Boyce, Russell / Jacobs, Peter et al. | Elsevier | 2006

      Validation study of numerical simulations by comparison to measurements in piston-driven shock-tunnels

      Mundt, Christian | Online Contents | 2007
      Beteiligte: Hannemann, Klaus

    Two-phase flow modeling combining the CICSAM with the projection method

    Gauer, Markus / Lambert, Markus / Kessler, Roland et al. | AIAA | 2012

    TIME-RESOLVED TEMPERATURE SENSITIVE PAINT MEASUREMENTS ON A HYPERSONIC INTAKE RAMP (AIAA 2018-5383)

    Laurence, Stuart J. / Ozawa, Hiroshi / Schramm, Jan Martinez et al. | British Library Conference Proceedings | 2018

    Time-resolved temperature sensitive paint measurements on a hypersonic intake ramp

    Laurence, Stuart J. / Ozawa, Hiroshi / Martinez Schramm, Jan et al. | AIAA | 2018

    Thermodynamic Interpretation of Cryogenic Injection Experiments

    Banuti, Daniel / Hannemann, Klaus | AIAA | 2011

    The Potential of Ultrasonically Absorptive TPS Materials for Hypersonic Vehicles (AIAA 2015-3576)

    Wagner, Alexander / Wartemann, Viola / Kuhn, Markus et al. | British Library Conference Proceedings | 2015

    The Potential of Ultrasonically Absorptive TPS Materials for Hypersonic Vehicles

    Wagner, Alexander / Wartemann, Viola / Kuhn, Markus et al. | AIAA | 2015

    Steady Shock Refraction in Hypersonic Ramp Flow

    Banuti, Daniel / Hannemann, Klaus | AIAA | 2011

    Simulation of LOx/GH2 single coaxial injector at high pressure conditions

    Fechter, Stefan / Karl, Sebastian / Hannemann, Volker et al. | AIAA | 2017

    Short Duration Force Measurements in Impulse Facilities

    Robinson, Matthew / Hannemann, Klaus | AIAA | 2006

    Shock Tube Testing of the Transpiration-Cooled Heat Shield Experiment AKTiV

    Boehrk, Hannah / Wartemann, Viola / Eggers, Thino et al. | AIAA | 2012

    Post Flight Analysis of SHEFEX I: Shock Tunnel Testing and Related CFD Analysis

    Martinez Schramm, Jan / Wagner, Alexander / Wolfram, Jeremy et al. | AIAA | 2009

    Numerische Simulation und stabilitätstheoretische Untersuchung des absolut und konvektiv instabilen Nachlaufs

    Hannemann, Klaus / Institut für Theoretische Strömungsmechanik, Deutsche Forschungs- und Versuchsanstalt für Luft- und Raumfahrt (DFVLR), Göttingen | TIBKAT | 1988

    Numerical Simulation of Liquid Rocket Engine Cooling Channels

    Bartolome Calvo, Javier / Hannemann, Klaus | AIAA | 2009

    Numerical Investigation of Space Launch Vehicle Base Flows with Hot Plumes

    Freier Zugriff
    Schumann, Jan-Erik / Fertig, Markus / Hannemann, Volker et al. | Springer Verlag | 2020