diff options
| 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/602data.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/602data.sci')
| -rwxr-xr-x | 548/DEPENDENCIES/602data.sci | 10 |
1 files changed, 10 insertions, 0 deletions
diff --git a/548/DEPENDENCIES/602data.sci b/548/DEPENDENCIES/602data.sci new file mode 100755 index 000000000..9546dfb23 --- /dev/null +++ b/548/DEPENDENCIES/602data.sci @@ -0,0 +1,10 @@ +//consider the CJ-1 at sea level.
+b=16.25;//wingspan(meter)
+S=29.54;//wingarea(m^2)
+AR=b^2/S;//aspect ratio
+D=1.225;//density at sea level(Kg/m^3)
+W=88176.75;//normal gross weight(N)
+Tf=2*16245//thrust (N) provided by two turbofan engine
+Cdo=0.02;//parasite drag coefficient
+e=0.81;//oswald efficiency factor
+V=linspace(40,300,500);//velocity over which we have to find thrust(40 to 300 m/s and over 500 points)
|