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

Mohd Razali, Mohd Aswadi (2009) Adjustable free boundary layer floor mechanism for UiTM aerospace wind tunnel / Mohd Aswadi Mohd Razali. Degree thesis, Universiti Teknologi MARA.

Abstract

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.

Metadata

Item Type: Thesis (Degree)
Creators:
Creators
Email / ID Num.
Mohd Razali, Mohd Aswadi
2005371040
Contributors:
Contribution
Name
Email / ID Num.
Thesis advisor
Wisnoe, Wirachman (Prof.Madya Dr.)
UNSPECIFIED
Subjects: T Technology > TL Motor vehicles. Aeronautics. Astronautics > Aeronautics. Aeronautical engineering
Divisions: Universiti Teknologi MARA, Shah Alam > Faculty of Mechanical Engineering
Keywords: Adjustable, Boundry, Floor, Aerospace wind tunnel
Date: 2009
URI: https://ir.uitm.edu.my/id/eprint/30908
Edit Item
Edit Item

Download

[thumbnail of 30908.pdf] Text
30908.pdf

Download (92kB)

Fulltext

Fulltext is available at:

ID Number

30908

Indexing

|

Statistic

Statistic details