Separation, stability, and other properties of compressible boundary layer with pressure gradient and heat transfer / Morris Morduchow and Richard C. Grape.
A theoretical study is made of the effect of pressure gradient, wall temperature, and Mach number on laminar boundary-layer characteristics and, in particular, on the skin-friction and heat-transfer coefficients, on the separation point in an adverse pressure gradient, on the wall temperature requir...
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Format: | Government Document Book |
Language: | English |
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Washington, D.C. :
National Advisory Committee for Aeronautics,
1955.
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Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
3296. National Advisory Committee for Aeronautics ; 3296. |
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Call Number: |
Y 3.N 21/5:6/3296
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Y 3.N 21/5:6/3296 | Available Place a Hold |