Comparison of theoretical and experimental heat transfer on a cooled 20 degree cone with a laminar boundary layer at a Mach number of 2.02 / Richard Scherrer and Forrest E. Gowen.
Heat-transfer measurements have been made on a cooled 20 degree cone with a laminar boundary layer at a Mach number of 2.02. Although the constant-temperature test region on the cone was preceded by severe surface-temperature gradients, a comparison of the results with the theory for a constant surf...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1950.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
2087. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/2087
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| Y 3.N 21/5:6/2087 | Available Place a Hold |