Flow Steadiness Over a Double Wedge at Mach 7 Including Effect of Trailing Edge Expansion
22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference
01.01.2018
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
British Library Conference Proceedings | 2018
|Dependence of Steady Mach Reflections on the Reflecting-Wedge Trailing-Edge Angle (TN)
Online Contents | 1997
|Separated trailing-edge flow at a transonic Mach number
AIAA | 1983
|Separated trailing-edge flow at a transonic Mach number
NTRS | 1983
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