Aerodynamics of micro aerial vehicle (MAV) / Muhd Hanif Hasan

MICRO AERIAL VEHICLE (MAV)...a quite strange name for those who had never heard it. To be more specific, it is a small size aircraft, flying in low speed and having mass less than lOOg. Based on that statement, our MAV design should follow the specifications but not totally at all. This project is a...

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Main Author: Hasan, Muhd Hanif
Format: Thesis
Language:English
Published: 2003
Online Access:https://ir.uitm.edu.my/id/eprint/73891/1/73891.pdf
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spelling my-uitm-ir.738912024-05-29T09:34:15Z Aerodynamics of micro aerial vehicle (MAV) / Muhd Hanif Hasan 2003 Hasan, Muhd Hanif MICRO AERIAL VEHICLE (MAV)...a quite strange name for those who had never heard it. To be more specific, it is a small size aircraft, flying in low speed and having mass less than lOOg. Based on that statement, our MAV design should follow the specifications but not totally at all. This project is attempted to make MAV and fly it. Based on that, we had design MAV, fabricate and test fly together with two groups of Diploma students. The dimension of MAV was 300 mm for span, 200 mm for chord. The weight was around 170g. After fabrication has been done, it was followed by test fly. The result was MAV failed to fly. Starting from there, the testing had been performed to find out the problems that cause the MAV couldn't fly. The results from the testing were used to make a new MAV. The purpose is to make sure that at this level the mission to fly MAV will be achieve. The dimension for the new design was 280 mm for span, 192 mm for root chord. The total weight is around 1 lOg. The design velocity at level flight had been set at lOm/s as well as 0.4 for lift coefficient (CL). This project will be continued by the next students. 2003 Thesis https://ir.uitm.edu.my/id/eprint/73891/ https://ir.uitm.edu.my/id/eprint/73891/1/73891.pdf text en public degree Universiti Teknologi MARA (UiTM) Faculty of Mechanical Engineering Mohamad, Nazri
institution Universiti Teknologi MARA
collection UiTM Institutional Repository
language English
advisor Mohamad, Nazri
description MICRO AERIAL VEHICLE (MAV)...a quite strange name for those who had never heard it. To be more specific, it is a small size aircraft, flying in low speed and having mass less than lOOg. Based on that statement, our MAV design should follow the specifications but not totally at all. This project is attempted to make MAV and fly it. Based on that, we had design MAV, fabricate and test fly together with two groups of Diploma students. The dimension of MAV was 300 mm for span, 200 mm for chord. The weight was around 170g. After fabrication has been done, it was followed by test fly. The result was MAV failed to fly. Starting from there, the testing had been performed to find out the problems that cause the MAV couldn't fly. The results from the testing were used to make a new MAV. The purpose is to make sure that at this level the mission to fly MAV will be achieve. The dimension for the new design was 280 mm for span, 192 mm for root chord. The total weight is around 1 lOg. The design velocity at level flight had been set at lOm/s as well as 0.4 for lift coefficient (CL). This project will be continued by the next students.
format Thesis
qualification_level Bachelor degree
author Hasan, Muhd Hanif
spellingShingle Hasan, Muhd Hanif
Aerodynamics of micro aerial vehicle (MAV) / Muhd Hanif Hasan
author_facet Hasan, Muhd Hanif
author_sort Hasan, Muhd Hanif
title Aerodynamics of micro aerial vehicle (MAV) / Muhd Hanif Hasan
title_short Aerodynamics of micro aerial vehicle (MAV) / Muhd Hanif Hasan
title_full Aerodynamics of micro aerial vehicle (MAV) / Muhd Hanif Hasan
title_fullStr Aerodynamics of micro aerial vehicle (MAV) / Muhd Hanif Hasan
title_full_unstemmed Aerodynamics of micro aerial vehicle (MAV) / Muhd Hanif Hasan
title_sort aerodynamics of micro aerial vehicle (mav) / muhd hanif hasan
granting_institution Universiti Teknologi MARA (UiTM)
granting_department Faculty of Mechanical Engineering
publishDate 2003
url https://ir.uitm.edu.my/id/eprint/73891/1/73891.pdf
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