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Numerical aerodynamic of the rectangular wing concerning to ground effect
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Heidarian, A, Ghassemi, H and Liu, P
ORCID: 0000-0003-2158-5442 2018
, 'Numerical aerodynamic of the rectangular wing concerning to ground effect'
, American Journal of Mechanical Engineering, vol. 6, no. 2
, pp. 43-47
, doi: 10.12691/ajme-6-2-1.

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Official URL: http://www.sciepub.com/ajme/abstract/8948
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.
Item Type: | Article |
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Authors/Creators: | Heidarian, A and Ghassemi, H and Liu, P |
Keywords: | ground effect, pressure and velocity distribution, lift and drag |
Journal or Publication Title: | American Journal of Mechanical Engineering |
Publisher: | Science and Education Publishing Co. Ltd. |
ISSN: | 2328-4102 |
DOI / ID Number: | 10.12691/ajme-6-2-1 |
Copyright Information: | ©Science and Education Publishing. Licensed under Creative Commons Attribution 4.0 International (CC BY 4.0) http://creativecommons.org/licenses/by/4.0/ |
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Item Statistics: | View statistics for this item |
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