A Simple and Robust Subsonic Boundary Layer Method to Be Used with the Panel Method for Wing Calculations Using a Wing Strip Approach

Publisher: Trans Tech Publications

E-ISSN: 1662-7482|2015|798|596-601

ISSN: 1660-9336

Source: Applied Mechanics and Materials, Vol.2015, Iss.798, 2015-11, pp. : 596-601

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Abstract