Aerodynamic performance and static stability at mach number 3.3 of an aircraft configuration employing three triangular wing panels and a body of equal length
1960
34 S
Ill., graph. Darst
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English
AERODYNAMIC PERFORMANCE OF A BLENDED-WING-BODY CONFIGURATION AIRCRAFT
British Library Conference Proceedings | 2006
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