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Weinacht, P. (2003) Prediction of Projectile Performance, Stability, and Free-Flight Motion Using Computational Fluid Dynamics. Tech. Rep. ARL-TR-3015, Army Research Laboratory.

has been cited by the following article:

• TITLE: Flow Field Investigation around Body Tail Projectile

  AUTHORS: Mahfouz Elnaggar Wessam, Zhihua Chen, Zhengui Huang

  KEYWORDS: Body Tail Projectile, Aerodynamic Coefficients, Viscosity, Flow Field

  JOURNAL NAME: Journal of Applied Mathematics and Physics, Vol.2 No.6, May 16, 2014

  ABSTRACT: 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.