Wind-tunnel investigation at low speed of the lateral control characteristics of ailerons having three spans and three trailing-edge angles on a semispan wing model /
Presents results of a wind-tunnel investigation of the low-speed lateral control characteristics of an essentiallty unswept wing (leading-edge sweptback 6.3 degrees) equipped with sealed 20-percent-chord plain ailerons having spans of 0.954, 0.583, and 0.294 percent of a full-span aileron, each with...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1948
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
1738 |
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| Call Number: |
NACA TN 1738 |
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