%0 Journal Article
%T Flow Field Investigation around Body Tail Projectile
%A Mahfouz Elnaggar Wessam
%A Zhihua Chen
%A Zhengui Huang
%J Journal of Applied Mathematics and Physics
%P 277-283
%@ 2327-4379
%D 2014
%I Scientific Research Publishing
%R 10.4236/jamp.2014.26033
%X <p class=\"MsoNormal\">
	<span lang=\"EN-US\">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.</span>
</p>
%K Body Tail Projectile
%K Aerodynamic Coefficients
%K Viscosity
%K Flow Field
%U http://www.scirp.org/journal/PaperInformation.aspx?PaperID=45938