1–20 von 35 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

    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
    Verlag: AIAA

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

    Laurence, Stuart J. / Ozawa, Hiroshi / Martinez Schramm, Jan et al. | AIAA | 2018
    Verlag: The American Institute of Aeronautics and Astronautics

    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
    Verlag: AIAA

    The Potential of Ultrasonically Absorptive TPS Materials for Hypersonic Vehicles

    Wagner, Alexander / Wartemann, Viola / Kuhn, Markus et al. | AIAA | 2015
    Verlag: The American Institute of Aeronautics and Astronautics

    Steady Shock Refraction in Hypersonic Ramp Flow

    Banuti, Daniel / Hannemann, Klaus | AIAA | 2011
    Verlag: The American Institute of Aeronautics and Astronautics

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

    Boehrk, Hannah / Wartemann, Viola / Eggers, Thino et al. | AIAA | 2012
    Verlag: The American Institute of Aeronautics and Astronautics

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

    Martinez Schramm, Jan / Wagner, Alexander / Wolfram, Jeremy et al. | AIAA | 2009
    Verlag: The American Institute of Aeronautics and Astronautics

    Passiv hypersonic boundary layer control by means of ultrasonically absorptive carbon-carbon ceramics: Investigations of different boundary conditions

    Wartemann, Viola / Wagner, Alexander / Eggers, Thino et al. | AIAA | 2015
    Verlag: The American Institute of Aeronautics and Astronautics

    Passive Hypersonic Boundary Layer Control by Means of Ultrasonically Absorptive Carbon-Carbon Ceramics: Investigations of Different Boundary Conditions (AIAA 2015-3577)

    Wartemann, Viola / Wagner, Alexander / Eggers, Thino et al. | British Library Conference Proceedings | 2015
    Verlag: AIAA

    Mixing and Combustion Enhancement in a Generic Combustion Chamber

    Mack, Andreas / Steelant, Johan / Hannemann, Klaus et al. | AIAA | 2006
    Verlag: The American Institute of Aeronautics and Astronautics

    Investigation of Unsteady/Quasi-Steady Scramjet Behavior using High-Speed Visualization Techniques

    Laurence, Stuart / Ozawa, Hiroshi / Lieber, Damien et al. | AIAA | 2012
    Verlag: The American Institute of Aeronautics and Astronautics

    Ground Testing Synthesis of the LAPCAT II Small Scale Flight Experiment Configuration Scramjet Flow Path (AIAA 2015-3627)

    Schramm, Jan Martinez / Hannemann, Klaus / Karl, Sebastian et al. | British Library Conference Proceedings | 2015
    Verlag: AIAA

    Ground Testing Synthesis of the LAPCAT II Small Scale Flight Experiment Configuration Scramjet Flow Path

    Martinez Schramm, Jan / Hannemann, Klaus / Karl, Sebastian et al. | AIAA | 2015
    Verlag: The American Institute of Aeronautics and Astronautics

    Ground Testing of the HyShot II Scramjet Configuration in HEG

    Martinez Schramm, Jan / Karl, Sebastian / Hannemann, Klaus et al. | AIAA | 2008
    Verlag: The American Institute of Aeronautics and Astronautics

    Free Flight Testing of a Scramjet Engine in a Large Scale Shock Tunnel (AIAA 2015-3608)

    Hannemann, Klaus / Schramm, Jan Martinez / Karl, Sebastian et al. | British Library Conference Proceedings | 2015
    Verlag: AIAA

    Free Flight Testing of a Scramjet Engine in a Large Scale Shock Tunnel

    Hannemann, Klaus / Martinez Schramm, Jan / Karl, Sebastian et al. | AIAA | 2015
    Verlag: The American Institute of Aeronautics and Astronautics

    Flow Control by Energy Deposition in Hypersonic Flow - Some Fundamental Considerations

    Banuti, Daniel / Hannemann, Klaus | AIAA | 2009
    Verlag: The American Institute of Aeronautics and Astronautics

    Experimental investigation of hypersonic boundary layer transition on a cone model in the High Enthalpy Shock Tunnel (HEG) at Mach 7.5

    Wagner, Alexander / Wartemann, Viola / Laurence, Stuart et al. | AIAA | 2011
    Verlag: The American Institute of Aeronautics and Astronautics

    Experimental investigation of hypersonic boundary-layer stabilization on a cone by means of ultrasonically absorptive carbon-carbon material

    Wagner, Alexander / Hannemann, Klaus / Kuhn, Markus | AIAA | 2012
    Verlag: The American Institute of Aeronautics and Astronautics