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

• Main Author: Che Wan Idris, Che Wan Zaidie
• Format: Thesis
• Language: English
• Published: 2009
• Subjects: Aeronautics. Aeronautical engineering
• Online Access: http://ir.uitm.edu.my/id/eprint/30866/1/30866.pdf; http://ir.uitm.edu.my/id/eprint/30866/

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...