Wind-tunnel Investigation of the Effects of Steady Rolling on the Aerodynamic Loading Characteristics of a 45© Sweptback Wing at High Subsonic Speeds

Wind-tunnel Investigation of the Effects of Steady Rolling on the Aerodynamic Loading Characteristics of a 45© Sweptback Wing at High Subsonic Speeds
Author: James W. Wiggins
Publisher:
Total Pages: 32
Release: 1954
Genre: Aerodynamic load
ISBN:
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Wind-tunnel Investigation of the Effects of Steady Rolling on the Aerodynamic Loading Characteristics of a 45© Sweptback Wing at High Subsonic Speeds
Language: en
Pages: 32

Wind-tunnel Investigation of the Effects of Steady Rolling on the Aerodynamic Loading Characteristics of a 45© Sweptback Wing at High Subsonic Speeds

Authors: James W. Wiggins
Categories: Aerodynamic load
Type: BOOK - Published: 1954 - Publisher:

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Wind-tunnel Investigation of the Effects of Steady Rolling on the Aerodynamic Loading Characteristics of a 45 Degree Sweptback Wing at High Subsonic Speeds
Language: en
Pages: 22

Wind-tunnel Investigation of the Effects of Steady Rolling on the Aerodynamic Loading Characteristics of a 45 Degree Sweptback Wing at High Subsonic Speeds

Authors: James W. Wiggins
Categories:
Type: BOOK - Published: 1953 - Publisher:

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Wind-tunnel Investigation to Determine the Horizontal- and Vertical-tail Contributions to the Static Lateral Stability Characteristics of a Complete-model Swept-wing Configuration at High Subsonic Speeds
Language: en
Pages: 692

Wind-tunnel Investigation to Determine the Horizontal- and Vertical-tail Contributions to the Static Lateral Stability Characteristics of a Complete-model Swept-wing Configuration at High Subsonic Speeds

Authors: James W. Wiggins
Categories: Airplanes
Type: BOOK - Published: 1956 - Publisher:

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An investigation was conducted in the Langley high-speed 7- by 10-foot tunnel to determine the horizontal- and vertical-tail contributions to the static lateral
Wind-tunnel Investigation at Low Speed of the Effect of Varying the Ratio of Body Diameter to Wing Span from 0.1 to 0.8 on the Aerodynamic Characteristics in Pitch of the 45© Sweptback-wing--body Combination
Language: en
Pages: 36

Wind-tunnel Investigation at Low Speed of the Effect of Varying the Ratio of Body Diameter to Wing Span from 0.1 to 0.8 on the Aerodynamic Characteristics in Pitch of the 45© Sweptback-wing--body Combination

Authors: Harold S. Johnson
Categories: Airplanes
Type: BOOK - Published: 1953 - Publisher:

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Wind-tunnel Investigation at High Subsonic Speeds of the Effect of Spoiler Profile on the Lateral Control Characteristics of a Wing-fuselage Combination Winter Quarter-chord Line Swept Back 32.6© and NACA 65A006 Airfoil Section
Language: en
Pages: 20

Wind-tunnel Investigation at High Subsonic Speeds of the Effect of Spoiler Profile on the Lateral Control Characteristics of a Wing-fuselage Combination Winter Quarter-chord Line Swept Back 32.6© and NACA 65A006 Airfoil Section

Authors: Harold S. Johnson
Categories: Airplanes
Type: BOOK - Published: 1953 - Publisher:

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