Investigation of boundary-layer transition on 10 degree cone in Langley 4- by 4-foot supersonic pressure tunnel at Mach numbers of 1.41, 1.61, and 2.01 / Archibald R. Sinclair anbd K.R. Czarnecki.
An investigation has been made to determine the transition Reynolds numbers on a 10 degree cone in the Langley 4- by 4-foot supersonic pressure tunnel at Mach numbers of 1.41, 1.61, and 2.01 and over a Reynolds number range from about 800,000 to 9,500,000 per foot. The results indicate that, on the...
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| Format: | Government Document Book |
| Language: | English |
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Washington, D.C. :
National Advisory Committee for Aeronautics,
1956.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
3648. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/3648
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| Y 3.N 21/5:6/3648 | Available Place a Hold |