Exploratory investigation of boundary-layer transition on a hollow cylinder at a Mach number of 6.9 / Mitchel H. Bertram.
The Reynolds number for transition on the outside of a hollow cylinder with heat transfer from the boundary layer to the wall has been investigated at a Mach number of 6.9 in the Langley 11-inch hypersonic tunnel. The type of boundary layer was determined from impact-pressure surveys. When only the...
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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) ;
3546. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/3546
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| Y 3.N 21/5:6/3546 | Available Place a Hold |