Studies on the Effects of Test Gas on the Flow Field around Large Angle Blunt Cone Flying at Hypersonic Mach Number
2002
Aufsatz (Zeitschrift)
Unbekannt
Flow Fields of a Large-Angle, Spiked Blunt Cone at Hypersonic Mach Numbers
Online Contents | 2005
|Inviscid hypersonic flow around blunt bodies
AIAA | 1965
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