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Showing results 1 to 1 of 1 Search took 0.00 seconds. Search: Posts Made By: pavitran

Forum: Main CFD Forum August 23, 2012, 12:02

Replies: 7 stagnation point at the trailing edge of the airfoil Views: 3,987 Posted By pavitran Hi I believe for incompressible flows Cp definition mathematically is written as: Cp=(p_node-p_infinity)/q_infinity Cp=(q_infinity-q_node)/q_infinity Cp=1-(q_node/q_infinity) Which implies...

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