Related Books

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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Scientific and Technical Aerospace Reports
Language: en
Pages: 970

Scientific and Technical Aerospace Reports

Authors:
Categories: Aeronautics
Type: BOOK - Published: 1975 - Publisher:

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Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the N
Tactical Missile Aerodynamics
Language: en
Pages: 731

Tactical Missile Aerodynamics

Authors:
Categories: Aeronautics
Type: BOOK - Published: 1992 - 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:
Type: BOOK - Published: 1958 - Publisher:

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Scientific and Technical Aerospace Reports
Language: en
Pages: 456

Scientific and Technical Aerospace Reports

Authors:
Categories: Aeronautics
Type: BOOK - Published: 1995 - Publisher:

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Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the N
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