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

Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70 Deg Swept Double-delta Wing at Mach Number 0.2
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Publisher :
Total Pages : 120
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ISBN-10 : NASA:31769000427347
ISBN-13 :
Rating : 4/5 (47 Downloads)

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

Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70 ̊swept Double-delta Wing at Mach Numbers from 1.50 to 2.86
Language: en
Pages: 88
Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70 ̊swept Double-delta Wing at Mach Number 0.2
Language: en
Pages: 86
Authors: Jim A. Penland
Categories: Aerodynamics, Supersonic
Type: BOOK - Published: 1978 - Publisher:

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