Study on the aerodynamics analysis for Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) using Computational Fluid Dynamics (CFD) for subsonic flow / Ridwan Mokhtar
Steady-state, three-dimensional CFD calculations were made for BWB model using the standard one-equation turbulence model, Spalart-Allmaras model of commercial code, FLUENT. Comparisons of aerodynamics characteristics which are lift coefficient, drag coefficient and pitching moment coefficient, pres...
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主要作者: | |
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格式: | Thesis |
语言: | English |
出版: |
2006
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在线阅读: | https://ir.uitm.edu.my/id/eprint/38934/1/38934.pdf |
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