Low-speed aerodynamic characteristics of airfoil sections with rounded trailing edges in forward and reverse flow /
Low-speed wind-tunnel tests were conducted to determine the two-dimensional aerodynamic characteristics of 6-, 12-, and 18-percent-thick airfoil sections with rounded trailing edges in both forward and reverse flow. The shapes incorporated camber with both the leading and trailing edges rounded to p...
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| Format: | Government Document Book |
| Language: | English |
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Washington, D.C. : Springfield, Va. :
National Aeronautics and Space Administration ; For sale by the National Technical Information Service [distributor],
1974
Washington, D.C. : [Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service], 1974 |
| Series: | NASA technical memorandum ;
3060 NASA technical memorandum X-3060 |
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