Pressure-distribution investigation of an N.A.C.A. 0009 airfoil with a 50-percent-chord plain flap and three tabs /
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| Main Authors: | , |
|---|---|
| Format: | Government Document Electronic eBook |
| Language: | English |
| Published: |
Washington, [D.C.] :
National Advisory Committee for Aeronautics,
1939.
|
| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
734. |
| Subjects: | |
| Online Access: | CONNECT |
