Boundary-layer transition at Mach 3.12 with and without single roughness elements / Paul F. Brinich.
Temperatures were measured on the external surface of a straight hollow cylinder alined [sic] parallel to the air stream. The stream Mach number was 3.12, the Reynolds number varied between 1,00,000 and 700,000 per inch, and there was negligible heat transfer between the cylinder and the stream. Fro...
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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) ;
3267. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/3267
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| Y 3.N 21/5:6/3267 | Available Place a Hold |