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author | prashantsinalkar | 2017-10-10 12:27:19 +0530 |
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committer | prashantsinalkar | 2017-10-10 12:27:19 +0530 |
commit | 7f60ea012dd2524dae921a2a35adbf7ef21f2bb6 (patch) | |
tree | dbb9e3ddb5fc829e7c5c7e6be99b2c4ba356132c /689/CH8/EX8.2/2.sce | |
parent | b1f5c3f8d6671b4331cef1dcebdf63b7a43a3a2b (diff) | |
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diff --git a/689/CH8/EX8.2/2.sce b/689/CH8/EX8.2/2.sce new file mode 100644 index 000000000..ef80c4492 --- /dev/null +++ b/689/CH8/EX8.2/2.sce @@ -0,0 +1,14 @@ +clc; funcprot(0);
+//Example 8.2 Lift Equation
+
+// Initialisation of variables
+V = 90*1.467; // Velocity in ft/s
+S = 300; //Wing Area.
+rho = 0.00237;
+W = 3000;
+
+// Calculations
+Cl = W*2/(rho*S*V^2); // From figure 8.8
+
+//Results
+disp("Corrosponding value of alpha for the above Lift Coefficient is 1.7 degree (from fig 8.8).",Cl,"Lift Coefficient for the above data is :");
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