Supercritical airfoil simulation -- CFD Online Discussion Forums

February 6, 2016, 09:53	Supercritical airfoil simulation	#1
Logha94 New Member Pragash Join Date: Feb 2016 Location: London Posts: 4 Rep Power: 10	i am carrying out 2D simulation on fluent using standard SST corrector and having an error when the hybrid solution is initialized as ' convergence tolerance of 1.000000e-06 not reached during Hybrid Initialization'. all the boundary conditions are set as 'pressure far-field' and aerofoil as 'wall'. operating pressure is zero and gauge pressure is 70155.24pa what could have gone wrong? thank you Last edited by Logha94; February 6, 2016 at 11:20.

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