Determining the velocity distribution in the boundary layer of an airfoil fitted with a rotary cylinder /
In the closer investigation of the results obtained from a wing model with a rotary cylinder mounted in its leading edge (NACA TM's 307 and 354), the velocity distribution in the vicinity of the surface of the model was determined by a hot-wire anemometer. The results confirmed the belief that...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington :
National Advisory Committee for Aeronautics,
1927
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| Series: | Technical memorandum (United States. National Advisory Committee for Aeronautics) ;
no. 411 |
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Internet
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| Call Number: |
NACA TM 411 |
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