Determination of control-surface characteristics from NACA plain-flap and tab data /
The data from previous NACA pressure-distribution investigations of plain flaps and tabs have been analyzed and are presented in this paper in a form readily applicable to the problems of control-surface design. The experimentally determined variation of aerodynamic parameters with flap chord and ta...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington D.C. :
National Advisory Committee for Aeronautics,
1941
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
796 |
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| Call Number: |
NACA TN 796 |
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