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authorprashantsinalkar2017-10-10 12:27:19 +0530
committerprashantsinalkar2017-10-10 12:27:19 +0530
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+clc; funcprot(0);
+//Example 8.15 Center of Pressure
+
+// Initialisation of variables
+WbyS = 8; //Wing Loading
+V = 100*1.467;
+CMo = -0.067;
+
+// Calculations
+Cl = (2*WbyS/(rho*V^2))
+CM_qtrChrd = CMo;
+CP = 0.25 - CM_qtrChrd/Cl;
+
+//Results
+disp(CP*100,"Center of Pressure in % of chord length:"); \ No newline at end of file