Downwash in the vertical and horizontal planes of symmetry behind a triangular wing in supersonic flow /
A method developed in a previous report for finding the induced velocity field behind a supersonic wing with well known load distribution is used to find the downwash behind a triangular wing with subsonic leading edges. Results are given for the chord plane in the extended vortex wake of the wing a...
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| Format: | Government Document Book |
| Language: | English |
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Washington, D.C. :
National Advisory Committee for Aeronautics,
1949
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
1803 |
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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: |
ISIL:US-CST NACA TN 1803 |
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