Discussion of the results of the boundary-layer tests of an airfoil fitted with a rotary cylinder /
The results of the velocity measurements in the boundary layer described in NACA-TM 411 are here discussed in greater detail. The measurements made were of the velocity distribution in the vicinity of an airfoil model fitted with a rotary cylinder and were undertaken for the purpose of obtaining a c...
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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. 424 |
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Internet
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| Call Number: |
NACA TM 424 |
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