The Aerodynamic characteristics of a model wing having a split flap deflected downward and moved to the rear /
Wind tunnel tests were made on a model wing with three different sized split trailing-edged flaps. The flaps were formed in the lower rear portion of the wing and wer rotated downward about axes at their front edges. The lift, drag, and center of pressure were measured with the axis in its original...
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| Format: | Government Document Book |
| Language: | English |
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Washington D.C. :
National Advisory Committee for Aeronautics,
1932
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
422 |
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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 422 |
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