Q:Vane initial field with tascflow.
Every specialist: I tried many times and couldn't get a convergent result when I calculate just one row of turbine vane with tascflow. I used pressure inlet condition and pressure outlet condition, the outlet Mach number should be 1.05 if it's convergent. How should I set up this problem?
Re: Q:Vane initial field with tascflow.
(1). Try to lower your exit Mach number first. (2). Run another case, to see whether you can get the flow field to converge at a lower Mach number. (3). If you still have problem, check with the support engineer.
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