Tunnel-wall corrections to rolling and yawing moments due to aileron deflection in closed rectangular wind tunnels / by Donald J. Graham.

A method is developed for calculating the tunnel-wall corrections to rolling and yawing moments due to aileron deflection on models in closed rectangular wind tunnels. Graphs are presented which permit a rapid determination of these corrections for models mounted in 7- by 10-foot or 8- by 12-foot wi...

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Bibliographic Details
Main Author: Graham, Donald J.
Corporate Authors: United States. National Advisory Committee for Aeronautics, Ames Research Center
Other title:NACA Wartime Reports. Series A.
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, [1945]
Series:Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. A14.
Subjects:
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