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

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 :
Publisher :
Total Pages : 81
Release :
ISBN-10 : OCLC:636444588
ISBN-13 :
Rating : 4/5 (88 Downloads)

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:


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