Further comparisons of theoretical and experimental lift and pressure distributions on airfoils in cascade at low-subsonic speed / S. Katzoff and Margery E. Hannah.
Comparisons of theoretical and experimental lift coefficients and pressure distributions were made for five compressor-type cascades of highly cambered NACA 6-series airfoils. The experimental lift coefficients were 0.2 and 0.4 less than the theoretical for the same mean-flow direction. When the the...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1951.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
2391. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/2391
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| Y 3.N 21/5:6/2391 | Available Place a Hold |