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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/6_17data.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/6_17data.sci')
| -rwxr-xr-x | 548/DEPENDENCIES/6_17data.sci | 17 |
1 files changed, 17 insertions, 0 deletions
diff --git a/548/DEPENDENCIES/6_17data.sci b/548/DEPENDENCIES/6_17data.sci new file mode 100755 index 000000000..c44970687 --- /dev/null +++ b/548/DEPENDENCIES/6_17data.sci @@ -0,0 +1,17 @@ +//for the jet power executive aircraft(CJ-1):
+W=88176.75;//normal gross weight(N)
+b=16.25;//wingspan(meter)
+S=29.54;//wingarea(m^2)
+AR=b^2/S;//aspect ratio
+e=0.81;//oswald efficiency factor
+h=1.83;//Height(m)of wing above ground
+D=1.225;//density at sea level(Kg/m^3)
+g=9.8;//Gravitational constant
+Ur=0.02;//Rolling friction coefficient
+Cl=1.0;//maximum lift coefficient during ground roll
+Cdo=0.02;//parasite drag coefficient
+T=32485;//thrust(N)
+phi=(16*h/b)^2/(1+(16*h/b)^2)//Ground effect factor
+Vlo=1.2*sqrt(2*W/(D*S*Cl))//liftoff velocity(1.2*Vstall in m/s)
+Dr=D*(0.7*Vlo)^2*S*(Cdo+phi*Cl^2/(%pi*e*AR))/2//drag(N)
+L=D*(0.7*Vlo)^2*S*Cl/2//lift(N)
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