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| author | priyanka | 2015-06-24 15:03:17 +0530 |
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| committer | priyanka | 2015-06-24 15:03:17 +0530 |
| commit | b1f5c3f8d6671b4331cef1dcebdf63b7a43a3a2b (patch) | |
| tree | ab291cffc65280e58ac82470ba63fbcca7805165 /548/DEPENDENCIES/5_02data.sci | |
| 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 '548/DEPENDENCIES/5_02data.sci')
| -rwxr-xr-x | 548/DEPENDENCIES/5_02data.sci | 11 |
1 files changed, 11 insertions, 0 deletions
diff --git a/548/DEPENDENCIES/5_02data.sci b/548/DEPENDENCIES/5_02data.sci new file mode 100755 index 000000000..eaa7c07a3 --- /dev/null +++ b/548/DEPENDENCIES/5_02data.sci @@ -0,0 +1,11 @@ +//consider the same wing configuration as that of example 5.1.
+L=700; //Lift per unit span
+V=50; // velocity of flow in test section(m/s)
+D=1.225;//standard sea level density,Kg/m^3
+q=D*V^2/2 //dynamic pressure,N/m^2
+S=1.3;//wing area,m^2
+Cl=L/(q*S) //coefficient of lift
+//from the value of Cl and wing configuration we can get angle of attack by using standard table:
+a=1 //angle of attack in degree
+//To cause zero lift Cl=0,so from standard table of Cl and Lift:
+a1=-2.2 //angle of attack in degree
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