An Experimental Study Of Unsteady Vortex / Turbulent Boundary Layer Interactions

The main aim of the present study is to investigate the performance of an oscillating sub boundary layer vortex generator (SBVG) through experimental approach. The current research work will focus on the interaction between turbulent boundary layer and SBVG. The vortex generator height, ℎ is approx...

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Main Author:	Haji Serakawi, Abdul Rashid
Format:	Thesis
Language:	English
Published:	2011
Subjects:	TL500-777 Aeronautics Aeronautical engineering
Online Access:	http://eprints.usm.my/43191/1/ABDUL%20RASHID%20HAJI%20SERAKAWI.pdf
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id	my-usm-ep.43191
record_format	uketd_dc
spelling	my-usm-ep.431912019-04-12T05:26:30Z An Experimental Study Of Unsteady Vortex / Turbulent Boundary Layer Interactions 2011-09 Haji Serakawi, Abdul Rashid TL500-777 Aeronautics. Aeronautical engineering The main aim of the present study is to investigate the performance of an oscillating sub boundary layer vortex generator (SBVG) through experimental approach. The current research work will focus on the interaction between turbulent boundary layer and SBVG. The vortex generator height, ℎ is approximately equal to 20% of the boundary layer thickness, �. The work is divided into two parts i.e. steady (passive) SBVG and oscillating (active) SBVG. The steady vortex was created by the static SBVG with angle of incidence, � of 18° with different vortex generator chord length, height, and spacing between vortex generators. In order to create unsteady vortex, the SBVG was oscillated at a number of frequencies. 2011-09 Thesis http://eprints.usm.my/43191/ http://eprints.usm.my/43191/1/ABDUL%20RASHID%20HAJI%20SERAKAWI.pdf application/pdf en public masters Universiti Sains Malaysia Pusat Pengajian Kejuteraan Aeroangkasa
institution	Universiti Sains Malaysia
collection	USM Institutional Repository
language	English
topic	TL500-777 Aeronautics Aeronautical engineering
spellingShingle	TL500-777 Aeronautics Aeronautical engineering Haji Serakawi, Abdul Rashid An Experimental Study Of Unsteady Vortex / Turbulent Boundary Layer Interactions
description	The main aim of the present study is to investigate the performance of an oscillating sub boundary layer vortex generator (SBVG) through experimental approach. The current research work will focus on the interaction between turbulent boundary layer and SBVG. The vortex generator height, ℎ is approximately equal to 20% of the boundary layer thickness, �. The work is divided into two parts i.e. steady (passive) SBVG and oscillating (active) SBVG. The steady vortex was created by the static SBVG with angle of incidence, � of 18° with different vortex generator chord length, height, and spacing between vortex generators. In order to create unsteady vortex, the SBVG was oscillated at a number of frequencies.
format	Thesis
qualification_level	Master's degree
author	Haji Serakawi, Abdul Rashid
author_facet	Haji Serakawi, Abdul Rashid
author_sort	Haji Serakawi, Abdul Rashid
title	An Experimental Study Of Unsteady Vortex / Turbulent Boundary Layer Interactions
title_short	An Experimental Study Of Unsteady Vortex / Turbulent Boundary Layer Interactions
title_full	An Experimental Study Of Unsteady Vortex / Turbulent Boundary Layer Interactions
title_fullStr	An Experimental Study Of Unsteady Vortex / Turbulent Boundary Layer Interactions
title_full_unstemmed	An Experimental Study Of Unsteady Vortex / Turbulent Boundary Layer Interactions
title_sort	experimental study of unsteady vortex / turbulent boundary layer interactions
granting_institution	Universiti Sains Malaysia
granting_department	Pusat Pengajian Kejuteraan Aeroangkasa
publishDate	2011
url	http://eprints.usm.my/43191/1/ABDUL%20RASHID%20HAJI%20SERAKAWI.pdf
_version_	1747821177785548800

An Experimental Study Of Unsteady Vortex / Turbulent Boundary Layer Interactions

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