Method for calculation of compressible laminar boundary layer with axial pressure gradient and heat transfer / Paul A. Libby and Morris Morduchow.
A rapid and sufficiently accurate method, for most practical purposes, of determining laminar-boundary-layer characteristics in flow with a given free-stream Mach number and given velocity distribution at the edge of the boundary layer is presented. The method can be easily applied to flow with zero...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1954.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
3157. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/3157
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| Y 3.N 21/5:6/3157 | Available Place a Hold |