1–20 von 68 Ergebnissen
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    Blunt body near-wake flow field at Mach 6

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

    Blunt body near-wake flow field at Mach 10

    Horvath, Thomas / Hannemann, Klaus | AIAA | 1997

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

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

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

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

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

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

    Short Duration Force Measurements in Impulse Facilities

    Robinson, Matthew / Hannemann, Klaus | AIAA | 2006

    CFD Analysis of the HyShot Supersonic Combustion Flight Experiment Configuration

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

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

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

    Mixing and Combustion Enhancement in a Generic Combustion Chamber

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

    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

    Ground Testing of the HyShot II Scramjet Configuration in HEG

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

    Numerical Simulation of Liquid Rocket Engine Cooling Channels

    Bartolome Calvo, Javier / Hannemann, Klaus | AIAA | 2009

    Implementation of the VOF Method in the DLR TAU Code

    Gauer, Markus / Hannemann, Volker / Hannemann, Klaus | AIAA | 2009

    Post Flight Analysis of SHEFEX I: Shock Tunnel Testing and Related CFD Analysis

    Martinez Schramm, Jan / Wagner, Alexander / Wolfram, Jeremy et al. | AIAA | 2009

    Combustion Experiments Performed Within the LAPCAT I Project - An Overview

    Hannemann, Klaus / Haidn, Oskar / Lamanna, Grazia et al. | AIAA | 2009

    Effect of Injector Wall Heat Flux on Cryogenic Injection

    Banuti, Daniel / Hannemann, Klaus | AIAA | 2010

    Interface advection with the TAU code and the CICSAM method on arbitrary grids

    Gauer, Markus / Hannemann, Klaus | Tema Archiv | 2010