Aerodynamic Characteristics Of A Hypersonic Research Airplane Concept Having A 70 Deg Swept Double Delta Wing At Mach Number 02

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Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70 Deg Swept Double-delta Wing at Mach Number 0.2

Author	:
Publisher	:
Total Pages	: 120
Release	: 1978
ISBN-10	: NASA:31769000427347
ISBN-13	:
Rating	: 4/5 ( Downloads)

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Book Synopsis Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70 Deg Swept Double-delta Wing at Mach Number 0.2 by :

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