Summary of experimental heat-transfer measurements in turbulent flow for a Mach number range from 0.87 to 5.05 / Maurice J. Brevoort and Barbara D. Arabian.
Heat-transfer measurements have been made in turbulent flow at Mach numbers varying from 0.87 to 5.05 and Reynolds numbers in the range from 1,000,000 to 950,000,000 through the use of an axially symmetric annular nozzle which consists of an inner shaped center body and an outer cylindrical sleeve....
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington :
National Advisory Committee for Aeronautics,
[1958]
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
4248. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/4248
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| Y 3.N 21/5:6/4248 | Available Place a Hold |