Adjustable free boundary layer floor mechanism for UiTM aerospace wind tunnel / Mohd Aswadi Mohd Razali

This project focuses on design and fabrication of an adjustable free boundary layer floor mechanism for Uitm's Aerospace Wind Tunnel. The devices will be used for wing in ground effect experiment. In order to conduct the actual experiment, the adjustable floor mechanism is needed to act as the...

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Bibliographic Details
Main Author:	Mohd Razali, Mohd Aswadi
Format:	Thesis
Language:	English
Published:	2009
Subjects:	Aeronautics Aeronautical engineering
Online Access:	https://ir.uitm.edu.my/id/eprint/30908/1/30908.pdf
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id	my-uitm-ir.30908
record_format	uketd_dc
spelling	my-uitm-ir.309082020-06-03T08:28:52Z Adjustable free boundary layer floor mechanism for UiTM aerospace wind tunnel / Mohd Aswadi Mohd Razali 2009 Mohd Razali, Mohd Aswadi Aeronautics. Aeronautical engineering This project focuses on design and fabrication of an adjustable free boundary layer floor mechanism for Uitm's Aerospace Wind Tunnel. The devices will be used for wing in ground effect experiment. In order to conduct the actual experiment, the adjustable floor mechanism is needed to act as the ground. The plate must be perfectly flat to make sure no lift is generated by the floor. The plate should be adjustable in terms of height. The aluminum rod thread was used to control movement of the plate. Four legs were used to hold the plate in horizontal position and to withstand force from the air flow. The device has been tested in the UiTM's wind tunnel and could sustain up to 45 m/s of wind speed. This thesis provides discussion through the design process of the model and fabrication of the prototype. A conclusion and recommendation is presented at the end of the report. 2009 Thesis https://ir.uitm.edu.my/id/eprint/30908/ https://ir.uitm.edu.my/id/eprint/30908/1/30908.pdf text en public degree Universiti Teknologi MARA Faculty of Mechanical Engineering Wisnoe, Wirachman (Prof.Madya Dr.)
institution	Universiti Teknologi MARA
collection	UiTM Institutional Repository
language	English
advisor	Wisnoe, Wirachman (Prof.Madya Dr.)
topic	Aeronautics Aeronautical engineering
spellingShingle	Aeronautics Aeronautical engineering Mohd Razali, Mohd Aswadi Adjustable free boundary layer floor mechanism for UiTM aerospace wind tunnel / Mohd Aswadi Mohd Razali
description	This project focuses on design and fabrication of an adjustable free boundary layer floor mechanism for Uitm's Aerospace Wind Tunnel. The devices will be used for wing in ground effect experiment. In order to conduct the actual experiment, the adjustable floor mechanism is needed to act as the ground. The plate must be perfectly flat to make sure no lift is generated by the floor. The plate should be adjustable in terms of height. The aluminum rod thread was used to control movement of the plate. Four legs were used to hold the plate in horizontal position and to withstand force from the air flow. The device has been tested in the UiTM's wind tunnel and could sustain up to 45 m/s of wind speed. This thesis provides discussion through the design process of the model and fabrication of the prototype. A conclusion and recommendation is presented at the end of the report.
format	Thesis
qualification_level	Bachelor degree
author	Mohd Razali, Mohd Aswadi
author_facet	Mohd Razali, Mohd Aswadi
author_sort	Mohd Razali, Mohd Aswadi
title	Adjustable free boundary layer floor mechanism for UiTM aerospace wind tunnel / Mohd Aswadi Mohd Razali
title_short	Adjustable free boundary layer floor mechanism for UiTM aerospace wind tunnel / Mohd Aswadi Mohd Razali
title_full	Adjustable free boundary layer floor mechanism for UiTM aerospace wind tunnel / Mohd Aswadi Mohd Razali
title_fullStr	Adjustable free boundary layer floor mechanism for UiTM aerospace wind tunnel / Mohd Aswadi Mohd Razali
title_full_unstemmed	Adjustable free boundary layer floor mechanism for UiTM aerospace wind tunnel / Mohd Aswadi Mohd Razali
title_sort	adjustable free boundary layer floor mechanism for uitm aerospace wind tunnel / mohd aswadi mohd razali
granting_institution	Universiti Teknologi MARA
granting_department	Faculty of Mechanical Engineering
publishDate	2009
url	https://ir.uitm.edu.my/id/eprint/30908/1/30908.pdf
_version_	1783734093202063360

Adjustable free boundary layer floor mechanism for UiTM aerospace wind tunnel / Mohd Aswadi Mohd Razali

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