M. Fischer, DAVID H. RUDY
Abstract
Slender cone boundary layer transition under angle of attack at Mach 21 with promoted leeward and fixed windward ray
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Slender cone boundary layer transition under angle of attack at Mach 21 with promoted leeward and fixed windward ray
Key concepts: Mach number, Angle of attack, Boundary layer, Cone (formal languages), Mechanics, Hypersonic speed, Mach wave, Physics