Reference values for a half missile body -- CFD Online Discussion Forums

March 24, 2024, 06:36	Reference values for a half missile body	#1
ghost_rider1145 New Member Join Date: Mar 2024 Posts: 3 Rep Power: 2	I am currently doing an external aerodynamics simulation of a wing body missile configuration and i am getting unsual values for the CL and CD, I am assuming some issue with the reference values, I have previously studied that for CD the Sref is the cross sectional area in this case half of it, but as CL depends on the area of wing fins etc, what should be Sref that i should give for correct computation

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