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Which approximations are made in case of panel method in case of subsonic problems?(a) Quadrilateral panels with constant source strength(b) Curved panels with constant source strength(c) Triangular panels with constant sink(d) Quadrilateral panels with constant sinkThis question was addressed to me in an interview.My enquiry is from General Three Dimensional Flows-Panel Techniques topic in division Three-Dimensional Incompressible Flow of Aerodynamics |
Answer» The correct choice is (a) Quadrilateral PANELS with constant source strength |
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