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Subsonic flow past thick wing in ground effect, lifting line theory

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In this paper the integral equation of the thick-wing theory in subsonic flow in the ground effect is obtained. In the same conditions the lifting line theory is also given.

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  1. L. Dragoş

    Present address: University of Bucharest, Str. Academiei 14, 70109, Bucharest, Romania

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    1. L. Dragoş
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    Dragoş, L. Subsonic flow past thick wing in ground effect, lifting line theory. Acta Mechanica 82, 49–60 (1990). https://doi.org/10.1007/BF01173739

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