naca-report-1208
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- November 2, 2016 Create Date
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National Advisory Committee for Aeronautics, Report - A Comparison of the Spanwise Loading Calculated by Various Methods with Experimental Loadings Obtained on a 45° Sweptback Wing of Aspect Ratio 8.02 at Reynolds Number of 4.0 x 10
| File | Action |
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| naca-report-1208 A Comparison of the Spanwise Loading Calculated by Various Methods with Experimental Loadings Obtained on a 45° Sweptback Wing of Aspect Ratio 8.02 at Reynolds.pdf | Download |
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