Drag Force on Axisymmetric Cone in Mach 5 Flow -- CFD Online Discussion Forums

February 28, 2011, 01:56	Drag Force on Axisymmetric Cone in Mach 5 Flow	#1
SleeperService New Member Join Date: Feb 2011 Posts: 10 Rep Power: 15	Hello all, I'm very new to Fluent, and for my thesis I am trying to calculate the drag force on a flared axisymmetric cone at zero AoA in hypersonic flow. I am unsure as to how to go about doing this. I have tried to compute a surface integral report of pressure coefficient, but I can't figure out how to get it to provide me with the axial force. I'm hoping somebody can help me with this. Thanks.

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