Longitudinal Stability and Wake-flow Characteristics of a Twisted and Cambered Wing-fuselage Combination of 45 Degree Sweepback and Aspect Ratio 8 with a Horizontal Tail and Stall-control Devices at a Reynolds Number of 4.0 X (10)6

Longitudinal Stability and Wake-flow Characteristics of a Twisted and Cambered Wing-fuselage Combination of 45 Degree Sweepback and Aspect Ratio 8 with a Horizontal Tail and Stall-control Devices at a Reynolds Number of 4.0 X (10)6
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Total Pages : 51
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ISBN-10 : OCLC:1109503079
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Rating : 4/5 (79 Downloads)

Book Synopsis Longitudinal Stability and Wake-flow Characteristics of a Twisted and Cambered Wing-fuselage Combination of 45 Degree Sweepback and Aspect Ratio 8 with a Horizontal Tail and Stall-control Devices at a Reynolds Number of 4.0 X (10)6 by : Gerald V. Foster

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Longitudinal Stability and Wake-flow Characteristics of a Twisted and Cambered Wing-fuselage Combination of 45 Degree Sweepback and Aspect Ratio 8 with a Horizontal Tail and Stall-control Devices at a Reynolds Number of 4.0 X (10)6 Related Books

Summary and Analysis of Horizontal-tail Contribution to Longitudinal Stability of Swept-wing Airplanes at Low Speeds
Language: en
Pages: 96
Authors: Robert H. Neely
Categories: Aeronautics
Type: BOOK - Published: 1959 - Publisher:

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