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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 /896/CH7/EX7.16 | |
| 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 '896/CH7/EX7.16')
| -rwxr-xr-x | 896/CH7/EX7.16/16.sce | 12 |
1 files changed, 12 insertions, 0 deletions
diff --git a/896/CH7/EX7.16/16.sce b/896/CH7/EX7.16/16.sce new file mode 100755 index 000000000..1690c5918 --- /dev/null +++ b/896/CH7/EX7.16/16.sce @@ -0,0 +1,12 @@ +clc
+//Example 7.16
+//calculate the verticle downward velocity of air hitting an aircraft wing
+l=15//m length of wing
+b=3//m thickness of wing
+A=l*b//m^2 area of the colliding surface of the wing
+rho_air=1.21//Kg/m^3
+Vx=50//m/s
+m=rho_air*A*Vx//Kg/s
+Fy=9810//N Weight of the aircraft
+Vy=Fy/m//m/s
+printf("The verticle downward velocity of air hitting the aircraft wing is %f m/s",Vy);
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