1–20 von 27 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

    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

    Adiabatic-compression Preheated Ludwieg Tube for the Realistic Simulation of Hypersonic Flows (AIAA 2015-3547)

    Chung, Joseph / Laurence, Stuart J. / Houim, Ryan W. | British Library Conference Proceedings | 2015
    Verlag: AIAA

    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

    A Roadmap for Obtaining and Implementing Heat Flux Measurements in the Hypersonic Environment

    Tiliakos, Nick T. / DeSorbo, Jeff / Martin, Nick et al. | AIAA | 2020
    Verlag: The American Institute of Aeronautics and Astronautics

    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

    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

    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

    Adiabatic-compression preheated Ludwieg tube for the realistic simulation of hypersonic flows

    Chung, Joseph / Laurence, Stuart J. | AIAA | 2015
    Verlag: The American Institute of Aeronautics and Astronautics

    OPTICAL FREE-FLIGHT MEASUREMENTS USING GPU-ACCELERATED COMPUTER GRAPHICS (AIAA 2018-5385)

    Starshak, William C. / Laurence, Stuart J. | British Library Conference Proceedings | 2018
    Verlag: AIAA

    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

    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

    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

    A TRANSIENT GLOBAL HEAT-FLUX MEASUREMENTS FOR HIGH-SPEED FLOW OVER A WALL-MOUNTED CYLINDER IN A SHOCK TUBE (AIAA 2018-5384)

    Ozawa, Hiroshi / Laurence, Stuart J. | British Library Conference Proceedings | 2018
    Verlag: AIAA

    An Experimental Investigation of Steady and Unsteady Combustion Phenomena in the HyShot II Combustor

    Laurence, Stuart / Martinez Schramm, Jan / Karl, Sebastian et al. | AIAA | 2011
    Verlag: The American Institute of Aeronautics and Astronautics