[cfd seeker]

hi all

i am trying to model hypersonic flow over 2D cone of length 0.5m, diameter 0.15838m and half cone angle of 9 degrees.

M.No=6.77
density based,implicit and steady solver
i have used Standard k-e,Realizable k-e and SST k-w turbulence models

During iterations it says temperature and pressure limited to default values(ofcourse that are in limit panel), sometimes it says time-step reduced in some cells due to excessive temperature change. After some iterations solution diverges and iterations stop by saying that floating point exception

I dont know where i am going wrong. Please give some suggestions as i am really stuckup.

I have to find CL,CD,CM values for 0 and 60 degrees angle of attack