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Numerical aerodynamic of the rectangular wing concerning to ground effect

Citation

Heidarian, A and Ghassemi, H and Liu, P, Numerical aerodynamic of the rectangular wing concerning to ground effect, American Journal of Mechanical Engineering, 6, (2) pp. 43-47. ISSN 2328-4102 (2018) [Refereed Article]


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Copyright Statement

©Science and Education Publishing. Licensed under Creative Commons Attribution 4.0 International (CC BY 4.0) http://creativecommons.org/licenses/by/4.0/

Official URL: http://www.sciepub.com/ajme/abstract/8948

DOI: doi:10.12691/ajme-6-2-1

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 Details

Item Type:Refereed Article
Keywords:ground effect, pressure and velocity distribution, lift and drag
Research Division:Engineering
Research Group:Aerospace Engineering
Research Field:Aerospace Structures
Objective Division:Manufacturing
Objective Group:Transport Equipment
Objective Field:Aerospace Equipment
UTAS Author:Liu, P (Associate Professor Pengfei Liu)
ID Code:124452
Year Published:2018
Deposited By:NC Maritime Engineering and Hydrodynamics
Deposited On:2018-02-22
Last Modified:2018-11-23
Downloads:29 View Download Statistics

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