Aerodynamic Characteristics at Mach Numbers from 0.33 to 1.20 of a Wing-body Design Concept for a Hypersonic Research Airplane

Aerodynamic Characteristics at Mach Numbers from 0.33 to 1.20 of a Wing-body Design Concept for a Hypersonic Research Airplane
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Total Pages : 84
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ISBN-10 : NASA:31769000425267
ISBN-13 :
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Book Synopsis Aerodynamic Characteristics at Mach Numbers from 0.33 to 1.20 of a Wing-body Design Concept for a Hypersonic Research Airplane by : James L. Dillon

Download or read book Aerodynamic Characteristics at Mach Numbers from 0.33 to 1.20 of a Wing-body Design Concept for a Hypersonic Research Airplane written by James L. Dillon and published by . This book was released on 1977 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:


Aerodynamic Characteristics at Mach Numbers from 0.33 to 1.20 of a Wing-body Design Concept for a Hypersonic Research Airplane Related Books

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