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Flow Field Investigation around Body Tail Projectile
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作者 mahfouz elnaggar wessam Zhihua Chen Zhengui Huang 《Journal of Applied Mathematics and Physics》 2014年第6期277-283,共7页
The unsteady compressible flow around a 50 mm projectile governed by the Navier-Stocks (NS) equation is numerically solved with a Large Eddy Simulation (LES) method, with the Sub-Grid Scale (SGS) solved by Smagorinsky... The unsteady compressible flow around a 50 mm projectile governed by the Navier-Stocks (NS) equation is numerically solved with a Large Eddy Simulation (LES) method, with the Sub-Grid Scale (SGS) solved by Smagorinsky-Lilly model. The computed results are obtained in supersonic flow regime for a viscous fluid in order to determine the aerodynamic coefficients with different angles of attack. The flow around a body tail projectile was solved as a three-dimensional flow. 展开更多
关键词 BODY TAIL PROJECTILE Aerodynamic COEFFICIENTS VISCOSITY Flow Field
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