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Jia, Q., W. Yang, and Z. Yang, Numerical study on aerodynamics of banked wing in ground effect. International Journal of Naval Architecture and Ocean Engineering, 2016. 8(2): p. 209-217.

has been cited by the following article:

Article

Numerical Aerodynamic of the Rectangular Wing Concerning to Ground Effect

1Department of Marine Engineering, Persian Gulf University, Boushehr, Iran

2Department of Maritime Engineering, Amirkabir University of Technology, Tehran, Iran

3Australian Maritime College, University of Tasmania, Australia


American Journal of Mechanical Engineering. 2018, Vol. 6 No. 2, 43-47
DOI: 10.12691/ajme-6-2-1
Copyright © 2018 Science and Education Publishing

Cite this paper:
Alireza Heidarian, Hassan Ghassemi, Pengfei Liu. Numerical Aerodynamic of the Rectangular Wing Concerning to Ground Effect. American Journal of Mechanical Engineering. 2018; 6(2):43-47. doi: 10.12691/ajme-6-2-1.

Correspondence to: Hassan  Ghassemi, Department of Maritime Engineering, Amirkabir University of Technology, Tehran, Iran. Email: gasemi@aut.ac.ir

Abstract

Numerical aerodynamic of the rectangular wing is presented regarding to the ground effect. Clark-Y wing section is selected for the present calculations. The Reynolds-averaged Navier-Stokes (RANS) equations solver of the ANSYS-CFX software is employed with a realizable k-ε turbulent model. The numerical results lift and drag of the rectangular airfoil at ground effect are verified with the experimental data. Pressure distribution and velocity contour and turbulent intensity at the trailing edge of the airfoil are presented and discussed.

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