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| author | prashantsinalkar | 2017-10-10 12:27:19 +0530 |
|---|---|---|
| committer | prashantsinalkar | 2017-10-10 12:27:19 +0530 |
| commit | 7f60ea012dd2524dae921a2a35adbf7ef21f2bb6 (patch) | |
| tree | dbb9e3ddb5fc829e7c5c7e6be99b2c4ba356132c /689/CH8/EX8.1 | |
| parent | b1f5c3f8d6671b4331cef1dcebdf63b7a43a3a2b (diff) | |
| download | Scilab-TBC-Uploads-7f60ea012dd2524dae921a2a35adbf7ef21f2bb6.tar.gz Scilab-TBC-Uploads-7f60ea012dd2524dae921a2a35adbf7ef21f2bb6.tar.bz2 Scilab-TBC-Uploads-7f60ea012dd2524dae921a2a35adbf7ef21f2bb6.zip | |
initial commit / add all books
Diffstat (limited to '689/CH8/EX8.1')
| -rw-r--r-- | 689/CH8/EX8.1/1.sce | 15 |
1 files changed, 15 insertions, 0 deletions
diff --git a/689/CH8/EX8.1/1.sce b/689/CH8/EX8.1/1.sce new file mode 100644 index 000000000..db929df26 --- /dev/null +++ b/689/CH8/EX8.1/1.sce @@ -0,0 +1,15 @@ +clc; funcprot(0);
+//Example 8.1 Lift Equation
+
+// Initialisation of variables
+V = 100*1.467; // Velocity in ft/s
+alpha =4;
+S = 250; //Wing Area.
+rho = 0.00237;
+
+// Calculations
+Cl = 0.649; // From figure 8.8
+W = Cl*rho/2*S*V^2;
+
+//Results
+disp(W,"Weight with which an airplane can fly with Clark Y wing (lb) :");
\ No newline at end of file |