Measurement of heat transfer in the turbulent boundary layer on a flat plate in supersonic flow and comparison with skin-friction results / C.C. Pappas.
Local heat-transfer rates on the surface of a heated flat plate at zero incidence to an air stream flowing at Mach numbers of 1.69 and 2.27 are presented. The Reynolds number range for both Mach numbers was 1,000,000 to 10,000,000. Surface temperatures were maintained near recovery temperature. It w...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1954.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
3222. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/3222
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| Y 3.N 21/5:6/3222 | Available Place a Hold |