CHARGE DISPUTE FORM
Cm = -0.0527 CD = 0.00545 => CDf = 0.00466 CDp = 0.00079. It provides the point of transition to turbulent flow in the upper and lower surfaces. It also provides CDf and CDp, the friction drag and pressure drag respectively. Getting a Hard Copy-----To get a copy in post script format of the displayed plot type.OPERv c> hard ................
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