Computational Investigation on the Effect of Fences on Aerodynamic Characteristics of an Aircraft Wing

Mohamed Hamdan. A

Title:
Computational Investigation on the Effect of Fences on Aerodynamic Characteristics of an Aircraft Wing

Authors:
Mohamed Hamdan. A

Cite This Article :

Mohamed Hamdan. A "Computational Investigation on the Effect of Fences on Aerodynamic Characteristics of an Aircraft Wing" Published in International Journal of Trend in Scientific Research and Development (ijtsrd), ISSN: 2456-6470, Volume-5 | Issue-4, June 2021, pp.1605-1610, URL: https://www.ijtsrd.com/papers/ijtsrd43687.pdf

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Abstract :
A computational study, to improve the stall characteristics of wing at high angles of attack, with and without fence configuration is done here. Wing fences, also known as boundary layer fences and potential fences are fixed aerodynamic devices attached to aircraft in the exactly middle of the span and two fences are fixed in the exactly middle of the wing span and two fences are fixed at 25 percentage of wing span from their corresponding wing tip. The main aim of this research is to improve the lift and stalling angle. A rectangular wing with different angles of attack is used. Modeling was done in CATIA V5 R20 and meshing and analyzing was taken in ANSYS workbench and CFX. Then the graph is drawn for CL and CD for various angles of attack and various models.

Keywords :
Stall, Lift, Fence and Configuration

Publication Details:

Unique Identification Number : IJTSRD43687

Published In : Volume-5 | Issue-4, June 2021

Page Number(s) : 1605-1610

Publisher Name : IJTSRD | www.ijtsrd.com | E-ISSN 2456-6470

Copyright © 2019 by author(s) and International Journal of Trend in Scientific Research and Development Journal. This is an Open Access article distributed under the terms of the Creative Commons Attribution License (CC BY 4.0) (http://creativecommons.org/licenses/by/4.0)

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