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This chapter extends the thin airfoil theory that was formulated in Chap. 3 to the case where the flow separates from the upper surface of the wing before it reaches the trailing edge. It demonstrates the diminutive effect of a limited separation on the integral aerodynamic forces.

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Partially Separated Wake

  • 章节

  • 发表日期：

    2025年

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  • Gil Iosilevskii

摘要

This chapter extends the thin airfoil theory that was formulated in Chap. 3 to the case where the flow separates from the upper surface of the wing before it reaches the trailing edge. It demonstrates the diminutive effect of a limited separation on the integral aerodynamic forces.