Calculated spanwise lift distributions and aerodynamic influence coefficients for unswept wings in subsonic flow / Franklin W. Diederich and Martin Zlotnick.
Spanwise lift distributions have been calculated for nineteen unswept wings with various aspect ratios and taper ratios and with a variety of angle-of-attack or twist distributions, including flap and aileron deflections, by means of the Weissinger methods with eight control points on the semispan....
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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) ;
3014. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/3014
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| Y 3.N 21/5:6/3014 | Available Place a Hold |