Experimental investigation at a Mach number of 2.41 of average skin-friction coefficients and velocity profiles for laminar and turbulent boundary layers and an assessment of probe effects / Robert M. O'Donnell.
An experimental investigation was made of laminar and turbulent boundary layers on the outer surface of a hollow cylinder at a Mach number of 2.41 and over a Reynolds number range of 60,00 to 950,000 per inch. Boundary-layer surveys were made by means of a total-pressure probe for stations ranging f...
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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) ;
3122. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/3122
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| Y 3.N 21/5:6/3122 | Available Place a Hold |