Theoretical loading at supersonic speeds of flat swept-back wings with interacting trailing and leading edges / Doris Cohen.
By the method of superposition of conical flows, the load distribution is calculated for regions of a long swept-back wing behind the points at which the Mach lines from the trailing-edge apex intersect the leading edge. It is found that a good approximation on the load can be obtained by the applic...
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| Other title: | Technical report archive and image library. |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1949.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
1991. |
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Internet
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| Call Number: |
Y 3.N 21/5:6/1991
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| Y 3.N 21/5:6/1991 | Available Place a Hold |