flow past a missle: how to solve divergence? -- CFD Online Discussion Forums

September 9, 2007, 22:53	flow past a missle: how to solve divergence?	#1
xiaofish Guest Posts: n/a	I am now using Spalart almarmas + 2nd order upwind to do simulations in FLUENT. but it is very fast to diverge after just a few steps of iterations. My mach number is around 2 and Reynolds number in order of 105. So how to solve the divergence problem? How can i get some reasonable initiation field for the iterations to continue? Thank you very much in advance!

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