Lift Drag And Static Longitudinal Stability Characteristics Of Configurations Consisting Of Three Triangular Wing Panels And A Body Of Equal Length At Mach Numbers From 300 To 628
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Lift, Drag, and Static Longitudinal Stability Characteristics of Configurations Consisting of Three Triangular Wing Panels and a Body of Equal Length at Mach Numbers from 3.00 to 6.28
Author | : Raymond C. Savin |
Publisher | : |
Total Pages | : 18 |
Release | : 1956 |
Genre | : Aerodynamics, Supersonic |
ISBN | : |
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Lift, Drag, and Static Longitudinal Stability Characteristics of Configurations Consisting of Three Triangular Wing Panels and a Body of Equal Length at Mach Numbers from 3.00 to 6.28 Related Books
Language: en
Pages: 18
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Type: BOOK - Published: 1956 - Publisher:
Lift, drag, and static-stability characteristics of a triangular-wing airplane were determined at Mach numbers from 3.00 to 6.28, angles of attack up to 13 degr
Language: en
Pages: 18
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Type: BOOK - Published: 1955 - Publisher:
Language: en
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The drag due to lift increases with increasing sweep through the Mach number range. Some increase in bag due to lift is evident decrease in taper ratio for wing