Aerodynamic Characteristics Of A Hypersonic Research Airplane Concept Having A 70 Deg Swept Double Delta Wing At Mach Numbers From 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 Deg Swept Double-delta Wing at Mach Numbers from 0.80 to 1.20, with Summary of Data from 0.20 to 6.0

Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70 Deg Swept Double-delta Wing at Mach Numbers from 0.80 to 1.20, with Summary of Data from 0.20 to 6.0
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Total Pages : 152
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ISBN-10 : NASA:31769000430291
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Rating : 4/5 ( Downloads)

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

Download or read book Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70 Deg Swept Double-delta Wing at Mach Numbers from 0.80 to 1.20, with Summary of Data from 0.20 to 6.0 written by and published by . This book was released on 1979 with total page 152 pages. Available in PDF, EPUB and Kindle. Book excerpt:


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

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