|February 27, 2006, 18:50||
Help with 2D supersonic impinging nozzle!!!!
Hi, I'm modelling a small 2D supersonic nozzle with flow impinging an infinite plate. Re=500000 Mach 3.5
When solving I am recieving a segmentation error after 580 iritations.
Similar models, with impingement distances equal to nozzle exit diameter, have run to 300000+ itr. Current model attempting impingement distances 3 times nozzle exit diameter.
Mesh is extremely fine at exit and impingement zone.
Let me know if you have any ideas or experience to get this thing going.
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