1–20 von 35 Ergebnissen
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    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

    Achievements Obtained for Sustained Hypersonic Flight within the LAPCAT-II project (AIAA 2015-3677)

    Steelant, Johan / Varvill, Richard / Defoort, Sebastien et al. | British Library Conference Proceedings | 2015
    Verlag: AIAA

    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

    Development of Ultra-fast Temperature Sensitive Paints for Hypersonic High Speed Flows (AIAA 2017-2211)

    Schramm, Jan Martinez / Edzards, Frank / Hannemann, Klaus | British Library Conference Proceedings | 2017
    Verlag: AIAA

    Achievements Obtained for Sustained Hypersonic Flight within the LAPCAT-II project

    Steelant, Johan / Varvill, Richard / Walton, Craig 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

    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

    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

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

    Cross Flow Phenomena in Streamline Traced Hypersonic Intakes

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

    Development of Ultra-fast Temperature Sensitive Paints for Hypersonic High Speed Flows

    Martinez Schramm, Jan / Edzards, Frank / Hannemann, Klaus | AIAA | 2017
    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

    Conceptual Design of the High-Speed Propelled Experimental Flight Test Vehicle HEXAFLY (AIAA 2015-3539)

    Steelant, Johan / Langener, Tobias / Di Matteo, F. et al. | British Library Conference Proceedings | 2015
    Verlag: AIAA

    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

    Enhancement of Free Flight Force Measurement Technique for Scramjet Engine Shock Tunnel Testing (AIAA 2017-2235)

    Hannemann, Klaus / Schramm, Jan Martinez / Karl, Sebastian et al. | British Library Conference Proceedings | 2017
    Verlag: AIAA

    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

    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

    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

    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