Design and CFD Analysis of Air Foil

B. Srinivas, Banoth Bhadru

Abstract


The CFD simulation results show close agreement with those of the experiments, thus suggesting a reliable alternative to experimental method in determining drag and lift. Three angles have been taken of NACA 0012 ie, 2 , 6, 8 degrees and there lift and drag is calculated using wind tunnel testing using ANSYS CFD fluent workbench and there results are compared with other inclination and there conclusion is drawn.

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Copyright (c) 2015 B. Srinivas, Banoth Bhadru

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