Aerodynamic Testing with Accelerometers in the High Enthalpy Shock Tunnel HIEST
46th, Aerospace sciences meeting AIAA ; 2008 ; Reno, NV
01.01.2008
6 pages
Aufsatz (Konferenz)
Englisch
Aerospace , AIAA , Aeronautics , Astronautics
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Influence of Thermal Non-Equilibrium on Nozzle Flow Condition of High Enthalpy Shock Tunnel HIEST
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