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Structural analysis and design of airplanes (1920)

United States. Army. Air Corps · [Washington] · leaf 139

An illustration from Structural analysis and design of airplanes, 1920, leaf 139
0 0.070 0.3000 0.100 0.3637 0.150 0.4350 0.200 0.4763 0.250 0.4900 0.300 0.5000 0.350 0.4950 0.400 0.4912 0.500 0.4675 0.600 0.4225 0.700 0.3612 0.800 0.2850 0.900 0.1887 0.950 0.1237 0.980 0.0762 0.990 0.0500 1.000 0.0000 Radius of Nose = .12 D 2 properties of the solid section may be accuratelv… … Fig. 77. Standard Strut Section The properties of the hollow streamline section of this contour maybe expressed in terms of the ratio of the mean length to the mean dia-meter. The mean length equals the outside length minus the thicknessof the tube, and the mean diameter equals the maximum outside…

Airplanes

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