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: |
| Summary: | 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 wind tunnels. The method is so developed that the corrections may be calculated for the deflection of either aileron alone or both ailerons simultaneously. |
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| Item Description: | NACA Wartime Report A-14. Originally issued as NACA Advance Restricted Report 4F21(January 1945) Prepared at the Ames Aeronautical Laboratory, Moffett Field, California. |
| Physical Description: | 28 pages, 5 unnumbered pages : illustrations ; 27 cm. |
| Bibliography: | Includes bibliographical references. |