Experimental aerodynamics of Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with elevator deflection of +15° and -15° using wind tunnel (Mach number 0.1-0.15) / Wan Mohd Hafizan Wan Razali

This thesis presents a study of aerodynamic of a Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with elevator deflection +15° and -15° using wind tunnel. This project is the continuation of previous research using Low Speed Tunnel LST and Computational Fluids Dynamics (CFD) simulation and is...

Full description

Saved in:
Bibliographic Details
Main Author: Wan Razali, Wan Mohd Hafizan
Format: Thesis
Language:English
Published: 2009
Subjects:
Online Access:https://ir.uitm.edu.my/id/eprint/36061/1/36061.pdf
Tags: Add Tag
No Tags, Be the first to tag this record!
id my-uitm-ir.36061
record_format uketd_dc
spelling my-uitm-ir.360612020-11-04T05:02:16Z Experimental aerodynamics of Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with elevator deflection of +15° and -15° using wind tunnel (Mach number 0.1-0.15) / Wan Mohd Hafizan Wan Razali 2009 Wan Razali, Wan Mohd Hafizan Machinery exclusive of prime movers Machine design and drawing This thesis presents a study of aerodynamic of a Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with elevator deflection +15° and -15° using wind tunnel. This project is the continuation of previous research using Low Speed Tunnel LST and Computational Fluids Dynamics (CFD) simulation and is very important to validate the result it. This project will present the Analysis of BWB Aerodynamics at low subsonic speed. The study will focus on the aerodynamic characteristics at various angles of attack at 0.1 Mach number using wind tunnel test. The objective of this project is to obtain the aerodynamic characteristics such as lift coefficient, drag coefficient and pitching moment coefficient of Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with elevator deflection +15° and -15° using wind tunnel and also to observe the quality of flow pattern around the BWB UAV at various angles of attack using flow visualization techniques. 2009 Thesis https://ir.uitm.edu.my/id/eprint/36061/ https://ir.uitm.edu.my/id/eprint/36061/1/36061.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 Machinery exclusive of prime movers
Machine design and drawing
spellingShingle Machinery exclusive of prime movers
Machine design and drawing
Wan Razali, Wan Mohd Hafizan
Experimental aerodynamics of Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with elevator deflection of +15° and -15° using wind tunnel (Mach number 0.1-0.15) / Wan Mohd Hafizan Wan Razali
description This thesis presents a study of aerodynamic of a Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with elevator deflection +15° and -15° using wind tunnel. This project is the continuation of previous research using Low Speed Tunnel LST and Computational Fluids Dynamics (CFD) simulation and is very important to validate the result it. This project will present the Analysis of BWB Aerodynamics at low subsonic speed. The study will focus on the aerodynamic characteristics at various angles of attack at 0.1 Mach number using wind tunnel test. The objective of this project is to obtain the aerodynamic characteristics such as lift coefficient, drag coefficient and pitching moment coefficient of Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with elevator deflection +15° and -15° using wind tunnel and also to observe the quality of flow pattern around the BWB UAV at various angles of attack using flow visualization techniques.
format Thesis
qualification_level Bachelor degree
author Wan Razali, Wan Mohd Hafizan
author_facet Wan Razali, Wan Mohd Hafizan
author_sort Wan Razali, Wan Mohd Hafizan
title Experimental aerodynamics of Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with elevator deflection of +15° and -15° using wind tunnel (Mach number 0.1-0.15) / Wan Mohd Hafizan Wan Razali
title_short Experimental aerodynamics of Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with elevator deflection of +15° and -15° using wind tunnel (Mach number 0.1-0.15) / Wan Mohd Hafizan Wan Razali
title_full Experimental aerodynamics of Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with elevator deflection of +15° and -15° using wind tunnel (Mach number 0.1-0.15) / Wan Mohd Hafizan Wan Razali
title_fullStr Experimental aerodynamics of Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with elevator deflection of +15° and -15° using wind tunnel (Mach number 0.1-0.15) / Wan Mohd Hafizan Wan Razali
title_full_unstemmed Experimental aerodynamics of Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) with elevator deflection of +15° and -15° using wind tunnel (Mach number 0.1-0.15) / Wan Mohd Hafizan Wan Razali
title_sort experimental aerodynamics of blended wing body (bwb) unmanned aerial vehicle (uav) with elevator deflection of +15° and -15° using wind tunnel (mach number 0.1-0.15) / wan mohd hafizan wan razali
granting_institution Universiti Teknologi MARA
granting_department Faculty of Mechanical Engineering
publishDate 2009
url https://ir.uitm.edu.my/id/eprint/36061/1/36061.pdf
_version_ 1783734322714378240