Pressure-distributioin investigation of an N.A.C.A. 0009 airfoil with an 80-percent-chord plain flap and three tabs /
Pressure-distribution tests of an N.A.C.A. 0009 airfoil with an 80-percent-chord plain flap and three tabs, having chords of 10, 20, and 30 percent of the flap chord, were made in the N.A.C.A. 4- by 6-foot vertical tunnel. Section data suitable for application to the design of horizontal and vertica...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington D.C. :
National Advisory Committee for Aeronautics,
1940
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
761 |
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| Call Number: |
NACA TN 761 |
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