Minimum-drag ducted and closed three-point body of revolution based on linearized supersonic theory / Hermon M. Parker.
The problem of the three-point body of revolution that has minimum wave drag, based on linearized supersonic-flow theory, has been solved formally without resort to slender-body approximations. The evaluation of the source-distribution function, as well as the body shape, requires numerical procedur...
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| Main Author: | |
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1956.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
3704. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/3704
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| Y 3.N 21/5:6/3704 | Available Place a Hold |