Comparison of supersonic combustion tests with shock tunnels, flight and CFD
Steelant, Johan and Mack, Andreas and Hannemann, Klaus and Gardner, Anthony Donald (2006) Comparison of supersonic combustion tests with shock tunnels, flight and CFD. 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, July 9-12, 2006, Sacramento, California.
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In 2002, the HyShot flight experiment was sucessfully launched and allowed to access experimental flight data for supersonic combustion. Ground based testing performed in the High Enthalpy Shock Tunnel (HEG) of the German Aerospace Center (DLR) allowed to reproduce the Mach 7.8 conditions. The present numerical work focuses on the computation of the experiments in the HEG considering flows with and without combustion and fuel injection. Further, variations of the equivalence ratio and the resulting influence on the flow topology are studied.
|Document Type:||Conference or Workshop Item (Paper)|
|Title:||Comparison of supersonic combustion tests with shock tunnels, flight and CFD|
|In ISI Web of Science:||No|
|Keywords:||scramjet, HEG, hypersonic, HyShot, CFD, TAU, combustion, hydrogen, turbulence, mixing, crossflow injection|
|Event Title:||42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit|
|Event Location:||Sacramento, California|
|Event Type:||international Conference|
|Event Dates:||July 9-12, 2006|
|HGF - Research field:||Aeronautics, Space and Transport|
|HGF - Program:||Space|
|HGF - Program Themes:||W - no assignement|
|DLR - Research area:||Space|
|DLR - Program:||W - no assignement|
|DLR - Research theme (Project):||W -- no assignement (old)|
|Institutes and Institutions:||Institute of Aerodynamics and Flow Technology > Spacecraft|
Institute of Aerodynamics and Flow Technology > High Speed Configurations
|Deposited By:||Dr. Anthony Gardner|
|Deposited On:||25 Jun 2007|
|Last Modified:||27 Apr 2009 13:52|
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