Doubts regarding cfd fluent -- CFD Online Discussion Forums

March 26, 2013, 09:37	Doubts regarding cfd fluent	#1
swathy09 New Member Join Date: Mar 2013 Posts: 1 Rep 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? Boundary Conditions: density based solver operating pressure 1atm temperature 2236k gauge pressure: 1.79979e08 pressure inlet and n pressure outlet condition n i used k-epsilon.

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