Numerical Aerodynamic of the Rectangular Wing Concerning to Ground Effect

Alireza Heidarian; Hassan Ghassemi; Pengfei Liu

doi:10.12691/ajme-6-2-1

Numerical Aerodynamic of the Rectangular Wing Concerning to Ground Effect

Alireza Heidarian
, Hassan Ghassemi
, Pengfei Liu

Research output: Contribution to journal › Article › Research

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.

Original language	English
Pages (from-to)	43-47
Number of pages	5
Journal	American Journal of Mechanical Engineering
Volume	6
Issue number	2
DOIs	https://doi.org/10.12691/ajme-6-2-1
Publication status	Published - 21 Apr 2024
Externally published	Yes

Keywords

ground effect
pressure and velocity distribution
lift and drag

Access to Document

10.12691/ajme-6-2-1Licence: CC BY

623647104-oaFinal published version, 454 KBLicence: CC BY

Cite this

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title = "Numerical Aerodynamic of the Rectangular Wing Concerning to Ground Effect",

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.",

keywords = "ground effect, pressure and velocity distribution, lift and drag",

author = "Alireza Heidarian and Hassan Ghassemi and Pengfei Liu",

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T1 - Numerical Aerodynamic of the Rectangular Wing Concerning to Ground Effect

AU - Heidarian, Alireza

AU - Ghassemi, Hassan

AU - Liu, Pengfei

PY - 2024/4/21

Y1 - 2024/4/21

N2 - 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.

AB - 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.

KW - ground effect

KW - pressure and velocity distribution

KW - lift and drag

U2 - 10.12691/ajme-6-2-1

DO - 10.12691/ajme-6-2-1

M3 - Article

SN - 2328-4110

VL - 6

SP - 43

EP - 47

JO - American Journal of Mechanical Engineering

JF - American Journal of Mechanical Engineering

IS - 2

ER -