124452 - Numerical aerodynamic of the rectangular wing concerning to ground effect.pdf (464.78 kB)
Numerical aerodynamic of the rectangular wing concerning to ground effect
journal contributionposted 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.
Publication titleAmerican Journal of Mechanical Engineering
Department/SchoolAustralian Maritime College
PublisherScience and Education Publishing Co. Ltd.
Place of publicationUSA
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/