This script calculates the lift induces drag properties of a three-dimensional wingarrow wing in potential flow. The planform geometry of the wing can bespecified for cases of symmetric wing loading about the center-line. | |||
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This script calculates the lift induces drag properties of a three-dimensional wingarrow wing in potential flow. The planform geometry of the wing can bespecified for cases of symmetric wing loading about the center-line. | |||
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