A Mathematical Derivation Method of the Aerodynamic Forces Effected on a Spatial Rod by Air Flow

The aerodynamic forces acting on the structural element of the incoming flow (liquid or gas) are among the most complex in nature in terms of defining both the module and the direction of their actions. This article attempts to display the aerodynamic loads acting on the space-curved rod of circular cross-section is directly related to the cross-section of a deformed rod basis, where the equilibrium equations of the rod are the most simple character.

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