Some Effects of Tail Height and Wing Plan Form on the Static Longitudinal Stability Characteristics of a Small-scale Model at High Subsonic Speeds

Some Effects of Tail Height and Wing Plan Form on the Static Longitudinal Stability Characteristics of a Small-scale Model at High Subsonic Speeds
Author: Albert G. Few
Publisher:
Total Pages: 80
Release: 1954
Genre: Airplanes
ISBN:
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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 wings having 300of sweep through most of the speed range.


Some Effects of Tail Height and Wing Plan Form on the Static Longitudinal Stability Characteristics of a Small-scale Model at High Subsonic Speeds
Language: en
Pages: 80

Some Effects of Tail Height and Wing Plan Form on the Static Longitudinal Stability Characteristics of a Small-scale Model at High Subsonic Speeds

Authors: Albert G. Few
Categories: Airplanes
Type: BOOK - Published: 1954 - Publisher:

GET EBOOK

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
Some Effects of Tail Height and Wing Plan Form on the Static Longitudinal Stability Characteristics of a Small-scale Model at High Subsonic Speeds
Language: en
Pages: 62

Some Effects of Tail Height and Wing Plan Form on the Static Longitudinal Stability Characteristics of a Small-scale Model at High Subsonic Speeds

Authors: Albert G. Few
Categories: Airplanes
Type: BOOK - Published: 1957 - Publisher:

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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
Static Longitudinal Characteristics at High Subsonic Speeds of a Complete Airplane Model with a Highly Tapered Wing Having the 0.80 Chord Line Unswept and with Several Tail Configurations
Language: en
Pages: 64

Static Longitudinal Characteristics at High Subsonic Speeds of a Complete Airplane Model with a Highly Tapered Wing Having the 0.80 Chord Line Unswept and with Several Tail Configurations

Authors: Kenneth W. Goodson
Categories: Stability of airplanes, Longitudinal
Type: BOOK - Published: 1961 - Publisher:

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An investigation was made at high subsonic speeds of a complete model having a highly tapered wing and several tail configurations. The basic aspect-ratio-4.00
Annual Report - National Advisory Committee for Aeronautics
Language: en
Pages:

Annual Report - National Advisory Committee for Aeronautics

Authors: United States. National Advisory Committee for Aeronautics
Categories: Aeronautics
Type: BOOK - Published: 1957 - Publisher:

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Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Index of NACA Technical Publications
Language: en
Pages: 388

Index of NACA Technical Publications

Authors: United States. National Advisory Committee for Aeronautics
Categories: Aeronautics
Type: BOOK - Published: 1959 - Publisher:

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