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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| Format: | Thesis |
| Language: | English |
| Published: |
2010
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| Subjects: | |
| Online Access: | https://ir.uitm.edu.my/id/eprint/36615/1/36615.pdf |
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