1–18 von 18 Ergebnissen
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    Calibration of Fast-Response Temperature Sensitive Paints for Their Application in Hypersonic High Enthalpy Flows

    Schramm, Jan Martinez / Edzards, Frank / Hannemann, Klaus | British Library Conference Proceedings | 2018

    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

    Hybrid RANS-LES Study of Transonic Flow in the Wake of a Generic Space Launch Vehicle

    Horchler, Tim / Oßwald, Kai / Hannemann, Volker et al. | British Library Conference Proceedings | 2018

    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

    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

    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

    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

    Experimental and Numerical Analysis of SHEFEX-II

    Barth, Tarik / Gehre, Rolf / Eggers, Thino et al. | Tema Archiv | 2013

    Application of Temperature and Pressure Sensitive Paints to DLR Hypersonic Facilities: ``Lessons Learned''

    Beck, Walter H. / Klein, Christian / Henne, Ulrich et al. | British Library Conference Proceedings | 2015

    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

    Design of an axisymmetric, contoured nozzle for the HEG

    Hannemann, Klaus / Institut für Theoretische Strömungsmechanik, Deutsche Forschungsanstalt für Luft- und Raumfahrt (DLR), Göttingen | TIBKAT | 1990

    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

    Launch Vehicle Base Flow Analysis Using Improved Delayed Detached-Eddy Simulation

    Lüdeke, Heinrich | Online Contents | 2015
    Beteiligte: Hannemann, Klaus

    Computational Analysis of Radiative Heat Loading on Hypervelocity Reentry Vehicles

    Karl, Sebastian | Online Contents | 2015
    Beteiligte: Hannemann, Klaus

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

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