Experimental aerodynamics of Blended Wing Body (BWB) unmanned aerial vehicle (UAV) with elevator deflection of +5° and -5° using wind tunnel (Mach number 0.1-0.15) / Che Wan Zaidie Che Wan Idris

Experimental aerodynamics of Blended Wing Body (BWB) unmanned aerial vehicle (UAV) with elevator deflection of +5° and -5° using wind tunnel (Mach number 0.1-0.15) / Che Wan Zaidie Che Wan Idris

This thesis presents a study of Aerodynamic of a Blended Wing Body (BWB) unmanned aerial vehicle (UAV) with elevator deflection using wind tunnel test. This project is the continuation of previous research using low speed wind tunnel test and the Computational Fluids Dynamics (CFD) simulation. The s...

Full description

Saved in:
Bibliographic Details
Main Author: Che Wan Idris, Che Wan Zaidie
Format: Thesis
Language:English
Published: 2009
Subjects:
Aeronautics
Aeronautical engineering
Online Access:https://ir.uitm.edu.my/id/eprint/30866/1/30866.pdf
Tags: Add Tag
No Tags, Be the first to tag this record!

Internet

https://ir.uitm.edu.my/id/eprint/30866/1/30866.pdf

Similar Items