Aerodynamic Characteristics Of A Hypersonic Research Airplane Concept Having A 70 Swept Double Delta Wing At Mach Numbers From 250 To 286

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Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70° Swept Double-delta Wing at Mach Numbers from 2.50 to 2.86

Author	: Jim A. Penland
Publisher	:
Total Pages	: 81
Release	: 1975
ISBN-10	: OCLC:636444588
ISBN-13	:
Rating	: 4/5 ( Downloads)

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Book Synopsis Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70° Swept Double-delta Wing at Mach Numbers from 2.50 to 2.86 by : Jim A. Penland

Download or read book Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70° Swept Double-delta Wing at Mach Numbers from 2.50 to 2.86 written by Jim A. Penland and published by . This book was released on 1975 with total page 81 pages. Available in PDF, EPUB and Kindle. Book excerpt: