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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 8.8 Polar Curves
+
+// Initialisation of variables
+W = 3000;
+S = 350;
+V = 90;
+rho = 0.002378;
+
+// Calculations
+Cl = 2*W/(S*V^2);
+Cd = 0.0561; //From figure 8.18
+HP = Cd*rho*S*V^3/(2*550);
+
+//Results
+disp(HP,"Horse power required by wing (hp) : "); \ No newline at end of file