Wind-tunnel investigation of the static lateral stability characteristics of wing-fuselage combinations at high supersonic speeds. : Taper-ratio series /

An investigation was conducted in the Langley high-speed 7- by 10-foot tunnel to determine the effects of variations in taper ratio within the range of 0.3 to 1.0 on the static lateral stability characteristics at high subsonic speeds of wing-fuselage combinations having wings of 45 degrees sweepbac...

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Bibliographic Details
Main Author: Wiggins, James W
Corporate Author: United States National Advisory Committee for Aeronautics
Other Authors: Fournier, Paul G
Format: Government Document Book
Language:English
Published: Washington : National Advisory Committee for Aeronautics, [1958]
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; 4174
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Stanford University

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Call Number: NACA TN 4174