41–60 von 68 Ergebnissen
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    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

    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

    Comparison of Supersonic Combustion Tests with Shock Tunnels, Flight and CFD

    Steelant, Johan / Mack, Andreas / Hannemann, Klaus et al. | AIAA | 2006

    CFD Analysis of the HyShot Supersonic Combustion Flight Experiment Configuration

    Karl, Sebastian / Hannemann, Klaus / Steelant, Johan et al. | AIAA | 2006

    Ground Testing of the HyShot II Scramjet Configuration in HEG

    Martinez Schramm, Jan / Karl, Sebastian / Hannemann, Klaus et al. | AIAA | 2008

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

    Laurence, Stuart / Ozawa, Hiroshi / Lieber, Damien et al. | AIAA | 2012

    Experimental Investigation of Supersonic Combustion in the HIEST and HEG Free Piston Shock Tunnels

    Martinez Schramm, Jan / Sunami, Tetsuji / Ito, Katsuhiro et al. | AIAA | 2010

    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

    Blunt body near-wake flow field at Mach 6

    Horvath, Thomas / McGinley, Catherine / Hannemann, Klaus | AIAA | 1996

    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

    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

    Conceptual Design of the High-Speed Propelled Experimental Flight Test Vehicle HEXAFLY

    Steelant, Johan / Langener, Tobias / Hannemann, Klaus et al. | AIAA | 2015

    High Frequency Free-Stream Disturbance Measurements in Hypersonic Wind Tunnels by Means of a Slender Wedge Probe

    Wagner, Alexander / Schuelein, Erich / Petervari, René et al. | AIAA | 2016

    Comparative Experiment on the Surface Catalysity in Two High Enthalpy Shock Tunnels

    Ueda, Shuichi / Weiland, Matthias / Itoh, Katsuhiro et al. | AIAA | 2004

    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

    Mixing and Combustion Enhancement in a Generic Combustion Chamber

    Mack, Andreas / Steelant, Johan / Hannemann, Klaus et al. | AIAA | 2006

    Cylinder Shock Layer Density Profiles Measured in High Enthalpy Flows in HEG

    Martinez Schramm, Jan / Hannemann, Klaus / Beck, Walter et al. | AIAA | 2002

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

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

    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