Influence of Thermal Non-Equilibrium on Nozzle Flow Condition of High Enthalpy Shock Tunnel HIEST
16th, AIAA International Space Planes and Hypersonic Systems and Technologies Conference ; 2009 ; Bremen, Germany
01.01.2009
9 pages
Includes bibliographic references and index
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Aerodynamic Testing with Accelerometers in the High Enthalpy Shock Tunnel HIEST
British Library Conference Proceedings | 2008
|