Theoretical and experimental investigation of the subsonic-flow fields beneath swept and unswept wings with tails of vortex-induced velocities / William J. Alford, Jr.
The flow-field characteristics beneath swept and unswept wings as determined by potential-flow theory are compared with the experimentally determined flow fields beneath swept and unswept wing-fuselage combinations. The potential-flow theory utilized considered both the spanwise and chordwise distri...
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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,
1956.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
3738. |
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Internet
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| Call Number: |
Y 3.N 21/5:6/3738
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| Y 3.N 21/5:6/3738 | Available Place a Hold |