Aditya, Armaan and Srinivas, G (2019) The numerical analysis of naca 0018 airfoil: Studying the effect of flap. International Journal of Mechanical and Production, 9 (4). pp. 1047-1054. ISSN 2249-6890
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Abstract
An airfoil is basically a cross-section of the wing or a blade (in case of rotor or propeller). Flap is such a device which is used to increase the amount of lift generated by an airfoil. As the flaps are deployed the curvature (or camber) of the
Item Type: | Article |
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Uncontrolled Keywords: | 2D Airfoil, ANSYS, CFD, Flap & Lift Coefficient |
Subjects: | Engineering > MIT Manipal > Aeronautical and Automobile |
Depositing User: | MIT Library |
Date Deposited: | 24 Jul 2019 04:52 |
Last Modified: | 24 Jul 2019 04:52 |
URI: | http://eprints.manipal.edu/id/eprint/154229 |
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