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This chapter sets a formal foundation of the thin airfoil theory, and presents a few basic solutions for aerodynamic loads acting on a thin wing sectionThin wing section in a steady flow. Its Appendix 2, which presents the most general solution of the particular singular integral equation, is central for Chaps. 4 , 8 , 9 and 11 .

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Thin Wing Sections in Steady Motion

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  • 发表日期：

    2025年

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  • Gil Iosilevskii

摘要

This chapter sets a formal foundation of the thin airfoil theory, and presents a few basic solutions for aerodynamic loads acting on a thin wing sectionThin wing section in a steady flow. Its Appendix 2, which presents the most general solution of the particular singular integral equation, is central for Chaps. 4 , 8 , 9 and 11 .