1–10 von 24 Ergebnissen
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    Modeling of Aluminum Particle Combustion in Solid Rocket Combustion Chambers

    Ecker, Tobias / Karl, Sebastian / Hannemann, Klaus | AIAA | 2017

    Simulation of LOx/GH2 single coaxial injector at high pressure conditions

    Fechter, Stefan / Karl, Sebastian / Hannemann, Volker et al. | AIAA | 2017

    Interfacial Area Modeling for Eulerian Spray Simulations in Liquid Rocket Engines

    Banuti, Daniel / Karl, Sebastian / Hannemann, Klaus | AIAA | 2008

    Computation of radiative and convective contributions to Viking afterbody heating

    Potter, Daniel F. / Karl, Sebastian / Lambert, Markus et al. | AIAA | 2013

    CFD Analysis of the HyShot II Scramjet Experiments in the HEG Shock Tunnel

    Karl, Sebastian / Hannemann, Klaus / Mack, Andreas et al. | AIAA | 2008

    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

    Cross Flow Phenomena in Streamline Traced Hypersonic Intakes

    Karl, Sebastian / Hannemann, Klaus / Steelant, Johan et al. | AIAA | 2015

    High Enthalpy Cylinder Flow in HEG: A Basis for CFD Validation

    Karl, Sebastian / Martinez Schramm, Jan / Hannemann, Klaus | AIAA | 2003

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

    Hannemann, Klaus / Martinez Schramm, Jan / Karl, Sebastian et al. | AIAA | 2015

    Computational Analysis of Radiative Heat Loading on Hypervelocity Reentry Vehicles

    Karl, Sebastian / Potter, Daniel / Lambert, Markus et al. | AIAA | 2014

      Computational Analysis of Radiative Heat Loading on Hypervelocity Reentry Vehicles

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