transonic rotor convergence problem -- CFD Online Discussion Forums

January 5, 2008, 05:30	transonic rotor convergence problem	#1
Noureddine Guest Posts: n/a	Hi all, I faced same convergence problem as posted before by Samad in this forum, with an indication that the maximum Mach number increase too much. I have used CFX-TurboGrid 11.0 for mesh generation and the Turbomachinery template for the CFX-PRE 11.00 I want to know if somebody have successful to get a convergence with a transonic compressor (rotor37 i my case)? and if yes, plz, tell how you did it ? any other advice is welcome Regards Noureddine

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