shocktube -- CFD Online Discussion Forums

July 18, 2007, 03:29	shocktube	#1
Shuo Guest Posts: n/a	Hello, I am testing a 2D code on the one dimensional shock tube problem. The numerical scheme is a second order flux splitting version of the MacCromick method (Beam & Warming). For some reason, the u and v velocity components are the same at each iteration. Shuo

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