Synthesis of an airfoil at supersonic Mach number
1965
IX, 92 S
graph. Darst
Grant no.: NsG-110-61
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Report
English
Rotorcraft Airfoil Performance Near Critical Mach Number
British Library Conference Proceedings | 2012
|Rotorcraft Airfoil Performance Near Critical Mach Number
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|Supersonic airfoil optimization
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