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March 2, 2014, 14:01 |
Integral Drag Coefficient
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Join Date: Mar 2014
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Hey all, i am trying to establish the integral drag coefficient of a 2D aerofoil by measuring the static pressures and velocities within the wake. The related experimental data can be found at 'An Experimental Investigation of a Supercritical Airfoil at Transonic Speeds' by Mateer et al. This report details the method however, it is not very clear to an non-expert like me.
I am using Fluent 14.5, can anyone help? |
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fluent drag, integral drag |
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