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This chapter extendsThin wing sectionin nonuniform motion the thin airfoil theory to the case where the motion of the wing is non-uniform. The aerodynamic forces acting on a wing section are obtained as convolutions of the transversal velocity of the wing and the gust through which the wing passes in the course of its motion with a pair of standard response functions. Properties of these functions are discussed..

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Thin Wing Sections in Non-uniform Motion

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  • 发表日期：

    2025年

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  • Gil Iosilevskii

摘要

This chapter extendsThin wing sectionin nonuniform motion the thin airfoil theory to the case where the motion of the wing is non-uniform. The aerodynamic forces acting on a wing section are obtained as convolutions of the transversal velocity of the wing and the gust through which the wing passes in the course of its motion with a pair of standard response functions. Properties of these functions are discussed..