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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/CH10/EX10.3/3.sce | |
parent | b1f5c3f8d6671b4331cef1dcebdf63b7a43a3a2b (diff) | |
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-rw-r--r-- | 689/CH10/EX10.3/3.sce | 16 |
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diff --git a/689/CH10/EX10.3/3.sce b/689/CH10/EX10.3/3.sce new file mode 100644 index 000000000..eff54bf58 --- /dev/null +++ b/689/CH10/EX10.3/3.sce @@ -0,0 +1,16 @@ +clc; funcprot(0);
+//Example 10.3 Correction for aspect ratio of monoplane
+
+// Initialisation of variables
+AR6 = 6;
+alp6 = 3;
+Cl = 0.381;
+Cd6 = 0.0170;
+AR4 = 4;
+
+// Calculations
+alp4 = alp6 - 18.24*Cl*(1/AR6 - 1/AR4);
+Cd4 = Cd6 - Cl^2*(1/%pi)*(1/AR6 - 1/AR4);
+
+//Results
+disp(Cd4,"Drag Coefficient at aspect ratio 4 :", alp4,"Angle of attack for aspect ration 4 :" );
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