|March 26, 2013, 09:37||
Doubts regarding cfd fluent
Join Date: Mar 2013
Posts: 1Rep Power: 0
I started a project on hypersonic speeds.Im new to the software and iv got doubts regarding the boundary condition.im trying to obtain the characteristics of a blunt body at mach 7.but every-time i plot, my cd range shoots up to 30000 and more,and shock is not captured either.Can anyone help me with the boundary condition?
density based solver
operating pressure 1atm
gauge pressure: 1.79979e08
pressure inlet and n pressure outlet condition
n i used k-epsilon.
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