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| author | priyanka | 2015-06-24 15:03:17 +0530 |
|---|---|---|
| committer | priyanka | 2015-06-24 15:03:17 +0530 |
| commit | b1f5c3f8d6671b4331cef1dcebdf63b7a43a3a2b (patch) | |
| tree | ab291cffc65280e58ac82470ba63fbcca7805165 /494/CH3/EX3.5 | |
| download | Scilab-TBC-Uploads-b1f5c3f8d6671b4331cef1dcebdf63b7a43a3a2b.tar.gz Scilab-TBC-Uploads-b1f5c3f8d6671b4331cef1dcebdf63b7a43a3a2b.tar.bz2 Scilab-TBC-Uploads-b1f5c3f8d6671b4331cef1dcebdf63b7a43a3a2b.zip | |
initial commit / add all books
Diffstat (limited to '494/CH3/EX3.5')
| -rwxr-xr-x | 494/CH3/EX3.5/3_5.sce | 15 |
1 files changed, 15 insertions, 0 deletions
diff --git a/494/CH3/EX3.5/3_5.sce b/494/CH3/EX3.5/3_5.sce new file mode 100755 index 000000000..501412ab8 --- /dev/null +++ b/494/CH3/EX3.5/3_5.sce @@ -0,0 +1,15 @@ +//all the quantities are expressed in SI units
+
+ratio = 12; //contraction ratio of wind tunnel nozzle
+Cl_max = 1.3; //maximum lift coefficient of the model
+S = 0.56; //wing planform area of the model
+L_max = 4448.22; //maximum lift force that can be measured by the mechanical balance
+rho_inf = 1.225; //free-stream density of air
+
+//the maximum allowable freestream velocity can be given as
+V_inf = sqrt(2*L_max/rho_inf/S/Cl_max);
+
+//thus the maximum allowable pressure difference is given by
+delta_p = 1/2*rho_inf*(V_inf^2)*(1-(ratio^-2));
+
+printf("\nRESULTS\n--------\nThe maximum allowable pressure difference between the wind tunnel setling chamber and the test section is\n delta_p = %4.2f Pa",delta_p)
\ No newline at end of file |