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

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 nu...

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Main Author: Idris, Mohamed Nizam Mohamed
Format: Monograph
Language:English
Published: Universiti Sains Malaysia 2021
Subjects:
Online Access:http://eprints.usm.my/54539/1/Evaluation%20Of%20The%20Mechanisms%20For%20Inducing%20Leading%20Edge%20Vortex%20Using%20Ansys%20Fluent.pdf
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spelling my.usm.eprints.54539 http://eprints.usm.my/54539/ Evaluation Of The Mechanisms For Inducing Leading Edge Vortex Using Ansys Fluent Idris, Mohamed Nizam Mohamed T Technology 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 Universiti Sains Malaysia 2021-06-01 Monograph NonPeerReviewed application/pdf en http://eprints.usm.my/54539/1/Evaluation%20Of%20The%20Mechanisms%20For%20Inducing%20Leading%20Edge%20Vortex%20Using%20Ansys%20Fluent.pdf 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 (Unpublished)
institution Universiti Sains Malaysia
building Hamzah Sendut Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Sains Malaysia
content_source USM Institutional Repository
url_provider http://eprints.usm.my/
language English
topic T Technology
spellingShingle T Technology
Idris, Mohamed Nizam Mohamed
Evaluation Of The Mechanisms For Inducing Leading Edge Vortex Using Ansys Fluent
description 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
format Monograph
author Idris, Mohamed Nizam Mohamed
author_facet Idris, Mohamed Nizam Mohamed
author_sort Idris, Mohamed Nizam Mohamed
title Evaluation Of The Mechanisms For Inducing Leading Edge Vortex Using Ansys Fluent
title_short Evaluation Of The Mechanisms For Inducing Leading Edge Vortex Using Ansys Fluent
title_full Evaluation Of The Mechanisms For Inducing Leading Edge Vortex Using Ansys Fluent
title_fullStr Evaluation Of The Mechanisms For Inducing Leading Edge Vortex Using Ansys Fluent
title_full_unstemmed Evaluation Of The Mechanisms For Inducing Leading Edge Vortex Using Ansys Fluent
title_sort evaluation of the mechanisms for inducing leading edge vortex using ansys fluent
publisher Universiti Sains Malaysia
publishDate 2021
url http://eprints.usm.my/54539/1/Evaluation%20Of%20The%20Mechanisms%20For%20Inducing%20Leading%20Edge%20Vortex%20Using%20Ansys%20Fluent.pdf
http://eprints.usm.my/54539/
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score 13.209306