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Numerical aerodynamic of the rectangular wing concerning to ground effect

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journal contribution
posted on 2023-05-19, 16:19 authored by Heidarian, A, Ghassemi, H, Pengfei Liu
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.

History

Publication title

American Journal of Mechanical Engineering

Volume

6

Pagination

43-47

ISSN

2328-4102

Department/School

Australian Maritime College

Publisher

Science and Education Publishing Co. Ltd.

Place of publication

USA

Rights statement

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

Repository Status

  • Open

Socio-economic Objectives

Aerospace equipment

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    University Of Tasmania

    Categories

    Keywords

    ground effectpressure and velocity distributionlift and drag

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    In Copyright

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