A study of boundary-layer transition and surface temperature distributions at Mach 3.12 / Paul F. Brinich.
Surface temperature distributions on a hollow cylinder alined with the airstream were studied in a Mach 3.12 wind tunnel at Reynolds numbers per inch from 100,000 to 700,000. Transition with and without single roughness elements was observed from the surface temperature distributions and from high-s...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1955.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
3509. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/3509
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| Y 3.N 21/5:6/3509 | Available Place a Hold |