Study of short period behaviour for BWB UAV / Mohd Safuan Rosli.

Rosli, Mohd Safuan (2009) Study of short period behaviour for BWB UAV / Mohd Safuan Rosli. Degree thesis, Universiti Teknologi MARA Shah Alam.

Abstract

This project presents a study of short period behavior of a Blended Wing Body Unmanned Aircraft Vehicle (BWB UAV). A previous study on BWB UAV preliminary design has been done. Information gathered related to BWB UAV and flight dynamic stability of aircraft has been carried out. This project began with literature study on the revolution of aircraft development, identification and introduction of aircraft anatomy, started to familiar with the basic formulation regarding to flight dynamic and stability. Furthermore, the study proceeds with the derivation of the short period approximation and followed by obtaining the analysis final result and taking a conclusion. It was found that the short period behavior of this BWB UAV as not effectively damped. It is important that short period behavior do a further analysis on flight dynamic stability and design which is beyond this project.

Metadata

Item Type: Thesis (Degree)
Creators:
Creators
Email / ID Num.
Rosli, Mohd Safuan
2006134919
Contributors:
Contribution
Name
Email / ID Num.
Thesis advisor
Kuntjoro, Wahyu (Prof. Dr.)
UNSPECIFIED
Subjects: T Technology > TL Motor vehicles. Aeronautics. Astronautics > Aeronautics. Aeronautical engineering > Mechanics of flight: Aerodynamics
Divisions: Universiti Teknologi MARA, Shah Alam > Faculty of Mechanical Engineering
Keywords: BWB, UAV, Short period behavior, aircraft vihicle
Date: 2009
URI: https://ir.uitm.edu.my/id/eprint/31573
Edit Item
Edit Item

Download

[thumbnail of 31573.pdf] Text
31573.pdf

Download (117kB)

Digital Copy

Digital (fulltext) is available at:

Physical Copy

Physical status and holdings:
Item Status:

ID Number

31573

Indexing

Statistic

Statistic details