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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Corporate Authors: | , |
Other title: | NACA Wartime Reports. Series A. |
Format: | Government Document Book |
Language: | English |
Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
[1945]
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Series: | Wartime Reports (United States. National Advisory Committee for Aeronautics) ;
no. A14. |
Subjects: |
Norlin Library - Basement - Government Information - US
Call Number: |
Y 3.N 21/5:11/A14
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Y 3.N 21/5:11/A14 | Available Place a Hold |