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Effect of Leading-edge Chord-extensions on the Aerodynamic Characteristics of a 45 Degrees Sweptback Wing-fuselage Combination at Mach Numbers of 0.40 to 1.03

Download or Read eBook Effect of Leading-edge Chord-extensions on the Aerodynamic Characteristics of a 45 Degrees Sweptback Wing-fuselage Combination at Mach Numbers of 0.40 to 1.03 PDF written by F.E. Jr West and published by . This book was released on 1953 with total page 40 pages. Available in PDF, EPUB and Kindle.
Effect of Leading-edge Chord-extensions on the Aerodynamic Characteristics of a 45 Degrees Sweptback Wing-fuselage Combination at Mach Numbers of 0.40 to 1.03
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Total Pages : 40
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ISBN-10 : OCLC:1109598017
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Rating : 4/5 (17 Downloads)

Book Synopsis Effect of Leading-edge Chord-extensions on the Aerodynamic Characteristics of a 45 Degrees Sweptback Wing-fuselage Combination at Mach Numbers of 0.40 to 1.03 by : F.E. Jr West

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Effect of Leading-edge Chord-extensions on the Aerodynamic Characteristics of a 45 Degrees Sweptback Wing-fuselage Combination at Mach Numbers of 0.40 to 1.03 Related Books

Investigation of the Effects of Leading-edge Chord-extensions and Fences in Combination with Leading-edge Flaps on the Aerodynamic Characteristics at Mach Numbers from 0.40 to 0.93 of a 45 Degree Sweptback Wing of Aspect Ratio 4
Language: en
Pages: 644
Authors: Kenneth P. Spreemann
Categories: Airplanes
Type: BOOK - Published: 1957 - Publisher:

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This investigation was made to determine the effects of 6 degree full-span and 3 degree partial-span leading-edge flaps in combination with chord-extensions or
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