Aerodynamic characteristics of a circular cylinder at Mach number 6.86 and angles of attack up to 90 degrees / Jim A. Penland.
Pressure-distribution and force tests of a circular cylinder have been made in the Langley 11-inch hypersonic tunnel at a Mach number of 6.88, a Reynolds number of 129,000, and angles of attack up to 90 degrees. The results are compared with the hypersonic approximation of Grimminger, Williams, and...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1957.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
3861. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/3861
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| Y 3.N 21/5:6/3861 | Available Place a Hold |