Supercritical 2D airfoil simulation with SST k-w model -- CFD Online Discussion Forums

February 6, 2016, 12:21	Supercritical 2D airfoil simulation with SST k-w model	#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

Posting Rules
You may not post new threads You may not post replies You may not post attachments You may not edit your posts BB code is On Smilies are On [IMG] code is On HTML code is Off Trackbacks are Off Pingbacks are On Refbacks are On Forum Rules

Similar Threads
Thread	Thread Starter	Forum	Replies	Last Post
Simulation of Axisymmetric Free Jet using LRR Reynolds Stress Model	skyinventorbt	OpenFOAM	1	January 2, 2022 18:42
k-omega SST simulation of turbulent flow around a circular cylinder	DanM	OpenFOAM Running, Solving & CFD	17	October 13, 2016 14:29
Simulation of 0021 airfoil at 120,000 Reynolds number	AUCH	FLUENT	0	September 25, 2013 00:05
Quenching simulation - wall boiling model	Michael.J	CFX	10	August 27, 2013 18:02
Problem with restart solution in shape_optimization.py	robyTKD	SU2 Shape Design	21	May 29, 2013 10:26

All times are GMT -4. The time now is 06:45.