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Charts for determining preliminary values of span-load, shear, bending-moment, and accumulated-torque distributions of swept wings of various taper ratios

机译:用于确定各种锥度比的后掠翼的跨度 - 载荷,剪切力,弯矩和累积 - 扭矩分布的初始值的图表

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Contains charts for use in determining preliminary values of the spanwise-load, shear, bending-moment, and accumulated-torque distributions of swept wings. The charts are based on strip theory and include four aerodynamic-load distributions, two section-moment distributions, and two inertia-load distributions. The taper ratios considered cover the range from 1.0 to 0 and the results are applicable to any angle of sweep.

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