Turbulent-heat-transfer measurements at a Mach number of 1.62 / Maurice J. Brevoort and Bernard Rashis.
Turbulent-heat-transfer measurements were obtained through the use of an axially symmetric annular nozzle which consists of an inner, shaped center body and an outer cylindrical sleeve. Measurements taken along the outer sleeve gave essentially flat-plate results that are free from wall interference...
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| Format: | Government Document Book |
| Language: | English |
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Washington, D.C. :
National Advisory Committee for Aeronautics,
1955.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
3461. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/3461
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| Y 3.N 21/5:6/3461 | Available Place a Hold |