The unsteady compressible flow around a body tail projectile is numerically solved with a
Large Eddy Simulation (LES) method, Smagorinsky-Lilly model was used as the Sub-Grid Scale (SGS). 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.
Relation:
Journal of Applied Science and Engineering 19(2),pp. 163-168
