Wind-tunnel Investigation at High Subsonic Speeds to Determine the Rolling Derivatives of Two Wing-fuselage Combinations Having Triangular Winds, Including a Semiempirical Method of Estimating the Rolling Derivatives

Wind-tunnel Investigation at High Subsonic Speeds to Determine the Rolling Derivatives of Two Wing-fuselage Combinations Having Triangular Winds, Including a Semiempirical Method of Estimating the Rolling Derivatives
Author: James W. Wiggins
Publisher:
Total Pages: 36
Release: 1954
Genre: Airplanes
ISBN:
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Wind-tunnel Investigation at High Subsonic Speeds to Determine the Rolling Derivatives of Two Wing-fuselage Combinations Having Triangular Winds, Including a Semiempirical Method of Estimating the Rolling Derivatives
Language: en
Pages: 36

Wind-tunnel Investigation at High Subsonic Speeds to Determine the Rolling Derivatives of Two Wing-fuselage Combinations Having Triangular Winds, Including a Semiempirical Method of Estimating the Rolling Derivatives

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

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Wind-tunnel Investigation of Effect of Sweep on Rolling Derivatives at Angles of Attack Up to 13 Degrees and at High Subsonic Mach Numbers, Including a Semiempirical Method of Estimating the Rolling Derivatives
Language: en
Pages: 47

Wind-tunnel Investigation of Effect of Sweep on Rolling Derivatives at Angles of Attack Up to 13 Degrees and at High Subsonic Mach Numbers, Including a Semiempirical Method of Estimating the Rolling Derivatives

Authors: James W. Wiggins
Categories: Airplanes
Type: BOOK - Published: 1958 - Publisher:

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An investigation was performed in the Langley high-speed 7- by 10-foot tunnel in order to determine the rolling derivatives for swept-wing-body configurations a
Wind-tunnel measurements at subsonic speeds of the static and dynamic-rotary stability derivatives of a triangular-wing airplane model having a triangular vertical tail
Language: en
Pages: 103

Wind-tunnel measurements at subsonic speeds of the static and dynamic-rotary stability derivatives of a triangular-wing airplane model having a triangular vertical tail

Authors: B.H. Beam
Categories: History
Type: BOOK - Published: - Publisher: Рипол Классик

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Wind-tunnel measurements at subsonic speeds of the static and dynamic-rotary stability derivatives of a triangular-wing airplane model having a triangular verti
Wind-tunnel Measurements and Estimated Values of the Rolling Stability Derivatives of a Variable-sweep Airplane Configuration at Subsonic and Transonic Speeds
Language: en
Pages: 32

Wind-tunnel Measurements and Estimated Values of the Rolling Stability Derivatives of a Variable-sweep Airplane Configuration at Subsonic and Transonic Speeds

Authors:
Categories:
Type: BOOK - Published: 1961 - Publisher:

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A Wind-tunnel Test Technique for Measuring the Dynamic Rotary Stability Derivatives Including the Cross Derivatives at High Mach Numbers
Language: en
Pages: 44

A Wind-tunnel Test Technique for Measuring the Dynamic Rotary Stability Derivatives Including the Cross Derivatives at High Mach Numbers

Authors: Benjamin H. Beam
Categories: Aerodynamics, Supersonic
Type: BOOK - Published: 1955 - Publisher:

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A method is described for measuring the dynamic stability derivatives of a model airplane in a wind tunnel. The characteristics features of this system are that