ABSTRACT
Computational Fluid Dynamics (CFD) is attractive to industry as it is more financially viable than the physical testing. In any case, one must note that the mind boggling stream reproduction is testing and blunder inclined and it takes a great deal of building ability to get approved arrangements. Applying the basic laws of mechanics to a liquid gives the overseeing conditions for a liquid. The protection of mass condition is
∂ ∂ + ∆ =( ) p t
u. ρ 0
where ρ = density; u = velocity and t = time The above conditions along with the protection of vitality condition frame an arrange-
ment of coupled and nonlinear fractional differential conditions. The design of the (Hendrick et al., 2008) HALE UAV is undertaken using Solidworks software for the surface design. A model was imported to an ANSYS ICEM CFD 15 in meshing tool. The model is imported as Para solid format for getting a fine meshing a model with 160,000 elements and 260,000 nodes, the interval counts are 500,250 and 100. The model is placed in a rectangular domain.
