A study of the stability of the laminar boundary layer as affected by changes in the boundary-layer thickness in regions of pressure gradient and flow through the surface / Neal Tetervin and David A. Levine.
Calculations made by the Schlichting method for computation of their critical Reynolds numbers demonstrate that in a region of falling pressure on an impervious surface an increase in boundary-layer thickness can cause the velocity profile shape to be changed enough by the increase in effective pres...
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| Format: | Government Document Book |
| Language: | English |
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Washington, D.C. :
National Advisory Committee for Aeronautics,
1952.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
2752. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/2752
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| Y 3.N 21/5:6/2752 | Available Place a Hold |