(t) of the airfoil in percentage of chord. For example, the NACA 2415 airfoil has a maximum thickness of 15% with a camber of 2% located 40% back from the airfoil leading edge (or 0.4c). Utilizing these m, p, and t values, we can compute the coordinates for an entire airfoil ...
Driss Z, Chelbi T, Kaffel A, Abid MS (2015) Experimental characterization of a NACA2415 airfoil wind turbine. In Haddar M, Abbes SM, Choley J-Y, Boukharouba T, Elnady T, Kanaev A, Ben Amar M, Chaari F (eds) Multiphysics modelling and simulation for systems design and monitoring: ...
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CFDVortex generetorNACA2415Front spoilerUsing of computational fluid dynamics (CFD) have big advanteges for design process components in the automotive industry. Flow structures around vehicle and drag forces can investigate in CFD...doi:10.1007/s12239-019-0088-6Bayindirli Cihan...