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1 article for “panel mehods”
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Transonic Flow Past Conically Cambered Wings
Abstract: The flow is analysed over conically cambered wings for transonic flow conditions. Wing Planform is conically cambered for supersonic flow for minimum induced drag. The circulation to determine the forces is developed using panel methods. Objective function for drag minima is formed using Lagrange multipliers. The transonic flow computations are progressed through computational fluid dynamics. In case of a subsonic leading edge in supersonic flow there is no shock wave …
Published in Journal of Aerospace Engineering & Technology · Vol. 3, Issue 1, 2013 · pp. 29–36 Read article