Evaluation Of The Mechanisms For Inducing Leading Edge Vortex Using Ansys Fluent

Idris, Mohamed Nizam Mohamed (2021) Evaluation Of The Mechanisms For Inducing Leading Edge Vortex Using Ansys Fluent. Project Report. Universiti Sains Malaysia, Pusat Pengajian Kejuruteraan Aeroangkasa. (Unpublished)

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Abstract

This thesis evaluates the mechanism for inducing leading edge vortex using synthetic jet utilising ansys fluent on an airfoil due to aerodynamic in the transitional Reynolds number regime. Two-dimensional simulations based on the concept of fluid-structure interaction at low-to-moderate Reynold’s number (6.77

Item Type: Monograph (Project Report)
Subjects: T Technology
Divisions: Kampus Kejuruteraan (Engineering Campus) > Pusat Pengajian Kejuruteraan Aeroangkasa (School of Aerospace Engineering) > Monograph
Depositing User: Mr Mohamed Yunus Mat Yusof
Date Deposited: 08 Sep 2022 02:00
Last Modified: 08 Sep 2022 02:00
URI: http://eprints.usm.my/id/eprint/54539

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