Aerodynamic Characteristics Of A Hypersonic Research Airplane Concept Having A 70 Swept Double Delta Wing At Mach Numbers 080 To 120 With Summary Of Data From 020 To 60

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Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70 Degree Swept Double-delta Wing at Mach Numbers Form 0.80 to 1.20, with Summary of Data from 0.20 to 6.0

Author	: Jim A. Penland
Publisher	:
Total Pages	: 144
Release	: 1979
ISBN-10	: OCLC:1109559864
ISBN-13	:
Rating	: 4/5 ( Downloads)

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Book Synopsis Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70 Degree Swept Double-delta Wing at Mach Numbers Form 0.80 to 1.20, with Summary of Data from 0.20 to 6.0 by : Jim A. Penland

Download or read book Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70 Degree Swept Double-delta Wing at Mach Numbers Form 0.80 to 1.20, with Summary of Data from 0.20 to 6.0 written by Jim A. Penland and published by . This book was released on 1979 with total page 144 pages. Available in PDF, EPUB and Kindle. Book excerpt: