Investigation of separation of the turbulent boundary layer / G.B. Schubauer and P.S. Klebanoff.
An investigation was conducted on a turbulent boundary layer near a smooth surface with pressure gradients sufficient to cause flow separation. The Reynolds number was high, but speeds were entirely within the incompressible flow range. The investigation consisted of measurements of mean flow, three...
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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,
1950.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
2133. |
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Internet
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| Call Number: |
Y 3.N 21/5:6/2133
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| Y 3.N 21/5:6/2133 | Available Place a Hold |