flux diverngence in simulating nasa rotor 67 using foam extend

mrezaprs · May 15, 2020, 04:08

hi
I hope you are well.
I'm simulating nasa Rotor67 in foam-extend using steadyCompresibleMRF solver.
after 7000 iteration , all of results converge to experimental design point , but max of flux divergence is still high and mach number is 0.1 higher than desgin point ( desgin point =1.38).
1- Is the flux diverngence important parameter to valdiate convergence?
2-how can I fix this parameter?
3- Do you have any idea to reduce the mach number ?
Screenshot from 2020-05-15 03-59-37.jpg

David King · September 15, 2022, 11:17

Hi, I am trying to simulate Rotor 67 in foam-extend, too. Can you help me about the boundary condition?

May 15, 2020, 04:08	flux diverngence in simulating nasa rotor 67 using foam extend	#1
mrezaprs New Member Join Date: Apr 2020 Posts: 1 Rep Power: 0	hi I hope you are well. I'm simulating nasa Rotor67 in foam-extend using steadyCompresibleMRF solver. after 7000 iteration , all of results converge to experimental design point , but max of flux divergence is still high and mach number is 0.1 higher than desgin point ( desgin point =1.38). 1- Is the flux diverngence important parameter to valdiate convergence? 2-how can I fix this parameter? 3- Do you have any idea to reduce the mach number ? Screenshot from 2020-05-15 03-59-37.jpg

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September 15, 2022, 11:17		#2
David King New Member Ji Ziqi Join Date: Jan 2022 Posts: 1 Rep Power: 0	Hi, I am trying to simulate Rotor 67 in foam-extend, too. Can you help me about the boundary condition?