[ANSYS Meshing] icem_structured -- CFD Online Discussion Forums

March 15, 2012, 06:41	icem_structured	#1
shanu iyer New Member shankar Join Date: Feb 2012 Posts: 6 Rep Power: 14	hello.. i have been working on an axi symmetric supersonic engine inlet. The inlet section is conical. Near the vertex of the cone only 3 edges are there which are to be mapped with 4 edges at the end of the cone. Also the cone has to be captured perfectly to analyze the shock wave. So please some one help me to get rid of this problem.

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