Longitudinal-stability Investigation of High-lift and Stall-control Devices on a 52 Degrees Sweptback Wing with and Without Fuselage and Horizontal Tail at a Reynolds Number of 6.8 X (10)6

Longitudinal-stability Investigation of High-lift and Stall-control Devices on a 52 Degrees Sweptback Wing with and Without Fuselage and Horizontal Tail at a Reynolds Number of 6.8 X (10)6
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Total Pages : 41
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ISBN-10 : OCLC:1109537517
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Rating : 4/5 (17 Downloads)

Book Synopsis Longitudinal-stability Investigation of High-lift and Stall-control Devices on a 52 Degrees Sweptback Wing with and Without Fuselage and Horizontal Tail at a Reynolds Number of 6.8 X (10)6 by : Gerald V. Foster

Download or read book Longitudinal-stability Investigation of High-lift and Stall-control Devices on a 52 Degrees Sweptback Wing with and Without Fuselage and Horizontal Tail at a Reynolds Number of 6.8 X (10)6 written by Gerald V. Foster and published by . This book was released on 1948 with total page 41 pages. Available in PDF, EPUB and Kindle. Book excerpt:


Longitudinal-stability Investigation of High-lift and Stall-control Devices on a 52 Degrees Sweptback Wing with and Without Fuselage and Horizontal Tail at a Reynolds Number of 6.8 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: 100
Authors: Robert H. Neely
Categories: Aeronautics
Type: BOOK - Published: 1959 - Publisher:

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Air-flow characteristics behind wings and wing-body combinations are described and are related to the downwash at specific tail locations for unseparated and se