Similar solutions for the compressible boundary layer on a yawed cylinder with transpiration cooling / by Ivan E. Beckwith.
Heat-transfer and skin-friction parameters obtained from exact solutions to the laminar compressible boundary-layer equations for infinite cylinders in yaw are presented. The effects of transpiration cooling, Prandtl number, pressure gradient, wall temperature, and viscosity relation were investigat...
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| Main Author: | |
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| Corporate Authors: | , |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Aeronautics and Space Administration,
1959.
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| Series: | NASA technical report ;
R-42. |
| Subjects: |
Norlin Library - Government Information - US
| Call Number: |
NAS 1.12:42
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| NAS 1.12:42 | Available Place a Hold |