Computational Fluids Dynamics (CFD) analysis of UiTM Blended Wing Body (BWB) Baseline-II UAV Model without Canard at Similar Reynolds and Mach Numbers with Wind Tunnel Test / Mohd Hafizi Idris

In this project paper, the aerodynamics analysis using Computational Fluid Dynamics (CFD) has been employed for Blended Wing Body (BWB) Baseline-II UAV Model without Canard at similar Reynolds and Mach numbers with wind Tunnel Test. The project was carrying out at 0.1 Mach number which is consider a...

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Bibliographic Details
Main Author: Idris, Mohd Hafizi
Format: Thesis
Language:English
Published: 2010
Subjects:
Online Access:http://ir.uitm.edu.my/id/eprint/36615/1/36615.pdf
http://ir.uitm.edu.my/id/eprint/36615/
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Institution: Universiti Teknologi Mara
Language: English

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