I need to help solving supersonic transverse flow and error
Dear all,
I'm doing a analysis of supersonic transverse flow with stinger shape injector. but i have lot of problem which is occured by error My problem is a compressible and 2 inlet and 1outlet. The conditions given to my problem are mainstream(air)
temperature limited to 1.000000e+00 in 7 cells on zone 16 time step reduced in 10 cells due to excessive temperature change (My coorant Number is 0.5, and also Positivity rate limit is 0.4) I want to know why this error is occured and how to solve this error. I wonder if there is anyone who could help me. Thanks, LJH |
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