Computational fluid dynamics (CFD) analysis of a blended wing body (BWB) unmanned aerial vehicle (UAV) with elevator deflection of - 15° (upward) at 0.1 and 0.3 mach number / Mohd. Fazil Jundam

Jundam, Mohd. Fazil (2009) Computational fluid dynamics (CFD) analysis of a blended wing body (BWB) unmanned aerial vehicle (UAV) with elevator deflection of - 15° (upward) at 0.1 and 0.3 mach number / Mohd. Fazil Jundam. Degree thesis, Universiti Teknologi MARA Shah Alam.

Abstract

This thesis represents the study on aerodynamics of a Blended Wing Body Unmanned Aircraft Ve-hicle (BWB UAV) at a low subsonic speed for elevator deflection of - 15°. Elevator is one of im-portant parts in aircraft desigbn where it can acts as a control surface that influencing the nose up and down during pitching motion of the aircraft. This project started with the construction of the BWB model and deflecting the elevator section into - 15° (Upward) by using CATIA V5 R16.

Metadata

Item Type:	Thesis (Degree)
Creators:	Creators Email / ID Num. Jundam, Mohd. Fazil 2006863814
Contributors:	Contribution Name Email / ID Num. Thesis advisor Wisnoe, Wirachman (Ass. Prof. Dr.) UNSPECIFIED
Subjects:	T Technology > TA Engineering. Civil engineering > Mechanics of engineering. Applied mechanics
Divisions:	Universiti Teknologi MARA, Shah Alam > Faculty of Mechanical Engineering
Programme:	Bachelor Engineering (Hons) (Mechanical)
Keywords:	Computational fluid dynamics, Blended wing body, Elevator deflection
Date:	2009
URI:	https://ir.uitm.edu.my/id/eprint/31242