Study on the aerodynamics analysis for Blended Wing Body (BWB) Unmanned Aerial Vehicle (UAV) using Computational Fluid Dynamics (CFD) for subsonic flow / Ridwan Mokhtar

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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書目詳細資料
主要作者:	Mokhtar, Ridwan
格式:	Thesis
語言:	English
出版:	2006
主題:	Control engineering systems Automatic machinery (General)
在線閱讀:	https://ir.uitm.edu.my/id/eprint/38934/1/38934.pdf
標簽:	添加標簽沒有標簽, 成為第一個標記此記錄!

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