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Enlist the computer methods used which benefitted the airfoil performance along with wind- tunnel testing.(a) Panel method(b) Advanced viscous flow solutions(c) Panel method and advanced viscous flow solutions(d) Hit – and – trial methodsI got this question in semester exam.My query is from Modern Low Speed Airfoils topic in chapter Incompressible Flow over Airfoils of Aerodynamics |
Answer» The correct OPTION is (c) Panel method and advanced VISCOUS flow solutions |
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