Investigation of laminar boundary layer in compressible fluids using the Crocco method / E.R. Van Driest.
The Crocco method has been used to compute the skin-friction and heat-transfer coefficients for high-speed air flow in the laminar boundary layer on the flat plate, assuming a Prandtl number of 0.75 and constant specific heat, and using the Sutherland viscosity law. The results are different from th...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1952.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
2597. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/2597
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| Y 3.N 21/5:6/2597 | Available Place a Hold |