21–40 von 76 Ergebnissen
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    Blunt body near-wake flow field at Mach 10

    Horvath, Thomas / Hannemann, Klaus | AIAA | 1997

    Visualization of Hypersonic Boundary-Layer Transition on a Slender Cone (Invited)

    Laurence, Stuart J. / Wagner, Alexander / Ozawa, Hiroshi et al. | AIAA | 2014

    Dynamic Mode Decomposition of Backward Facing Step Flow Simulation Data

    Horchler, Tim / Mani, Karthik V. / Hannemann, Klaus | AIAA | 2015

    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

    Computation of radiative and convective contributions to Viking afterbody heating

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

    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

    Interfacial Area Modeling for Eulerian Spray Simulations in Liquid Rocket Engines

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

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

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

    Force and Moment Measurements on a Free-Flying Capsule Model in a High-Enthalpy Shock Tunnel

    Laurence, Stuart / Martinez Schramm, Jan / Hannemann, Klaus | AIAA | 2012

    The Potential of Ultrasonically Absorptive TPS Materials for Hypersonic Vehicles

    Wagner, Alexander / Wartemann, Viola / Kuhn, Markus 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

    Cross Flow Phenomena in Streamline Traced Hypersonic Intakes

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

    CFD Analysis of Unstart Characteristics of the HyShot-II Scramjet Configuration in the HEG Shock Tunnel

    Karl, Sebastian / Martinez Schramm, Jan / Hannemann, Klaus et al. | AIAA | 2011

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

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

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

    Steelant, Johan / Varvill, Richard / Walton, Craig et al. | AIAA | 2015

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

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

    Time-resolved temperature sensitive paint measurements on a hypersonic intake ramp

    Laurence, Stuart J. / Ozawa, Hiroshi / Martinez Schramm, Jan et al. | AIAA | 2018

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

    Mundt, Christian / Boyce, Russell / Jacobs, Peter et al. | Elsevier | 2006

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

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

    Two-phase flow modeling combining the CICSAM with the projection method

    Gauer, Markus / Lambert, Markus / Kessler, Roland et al. | AIAA | 2012