The drag of finite-length cylinders determined from flight tests at high Reynolds numbers for a Mach number range from 0.5 to 1.3 / Clement J. Welsh.
Reults of a free-flight investigation to determine the drg of circular, finite-length cylinders are presented for a Mach number range from about 0.5 to 1.3. Fineness ratios of the cylinders tested were 15, 30, and 60. Results of previous experimental tests of circular cylinders having infinite finen...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1953.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
2941. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/2941
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| Y 3.N 21/5:6/2941 | Available Place a Hold |