Effect Of Wing Flexibility On The Damping In Roll Of A Notched Delta Wing Body Combination Between Mach Numbers 06 And Approximately 22 As Determined With Rocket Propelled Models

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Effect of Wing Flexibility on the Damping in Roll of a Notched Delta Wing Body Combination Between Mach Numbers 0.6 and Approximately 2.2 as Determined with Rocket-propelled Models

Author	: William M. Bland
Publisher	:
Total Pages	: 20
Release	: 1954
ISBN-10	: OCLC:1109516006
ISBN-13	:
Rating	: 4/5 ( Downloads)

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Book Synopsis Effect of Wing Flexibility on the Damping in Roll of a Notched Delta Wing Body Combination Between Mach Numbers 0.6 and Approximately 2.2 as Determined with Rocket-propelled Models by : William M. Bland

Download or read book Effect of Wing Flexibility on the Damping in Roll of a Notched Delta Wing Body Combination Between Mach Numbers 0.6 and Approximately 2.2 as Determined with Rocket-propelled Models written by William M. Bland and published by . This book was released on 1954 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt: