Aerodynamic effects of a split flap on the spinning characteristics of a monoplane model /
The investigation described in this report was made to determine the change in aerodynamic forces and moments produced by split flaps in a steady spin. The tests were made with the spinning balance in the N.A.C.A. 5-foot verical wind tunnel. A low-wing monoplane model was tested with and without spl...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington D.C. :
National Advisory Committee for Aeronautics,
1934
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
515 |
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Internet
This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.Stanford University
| Call Number: |
NACA TN 515 |
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