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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 /548/DEPENDENCIES/4_03data.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/4_03data.sci')
| -rwxr-xr-x | 548/DEPENDENCIES/4_03data.sci | 8 |
1 files changed, 8 insertions, 0 deletions
diff --git a/548/DEPENDENCIES/4_03data.sci b/548/DEPENDENCIES/4_03data.sci new file mode 100755 index 000000000..8da6c5376 --- /dev/null +++ b/548/DEPENDENCIES/4_03data.sci @@ -0,0 +1,8 @@ +//Application of Bernoulli's equation.an airfoil placed in a flow of air
+P1=1.013;//pressure at far upstream of airfoil in bar
+V1=160*5/18 //velocity at far upstream of airfoil in m/s
+D=1.23;//density at far upstream of airfoil in Kg/m^3
+Pa=0.99;//pressure at a point Aon airfoil in bar
+//velocity is low enough so we can assume incompressible flow,so
+disp("P1+(D*V1^2/2)=Pa+(D*V2^2/2)","Bernoulli equation");
+Va=[(2*(P1-Pa)/D)+(V1)^2]^0.5
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