Measurements of the nonlinear variation with temperature of heat-transfer rate from hot wires in transonic and supersonic flow / Warren Winovich and Howard A. Stine.
Equilibrium temperatures and heat-transfer rates for 0.00015- and 0.00030-inch diameter tungsten wires normal to the flow were determined throughout the Mach number range 0.5 to 2.5 with Reynolds number 0.5 to 2.5 with Reynolds number varying between the limits 18 and 144. This test range correspond...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington :
National Advisory Committee for Aeronautics,
[1957]
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
3965. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/3965
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| Y 3.N 21/5:6/3965 | Available Place a Hold |