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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_4b_data.sci | |
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initial commit / add all books
Diffstat (limited to '548/DEPENDENCIES/6_4b_data.sci')
-rwxr-xr-x | 548/DEPENDENCIES/6_4b_data.sci | 12 |
1 files changed, 12 insertions, 0 deletions
diff --git a/548/DEPENDENCIES/6_4b_data.sci b/548/DEPENDENCIES/6_4b_data.sci new file mode 100755 index 000000000..0f9234cfc --- /dev/null +++ b/548/DEPENDENCIES/6_4b_data.sci @@ -0,0 +1,12 @@ +//for the jet power executive aircraft(CJ-1):
+Tf=2*16245;//thrust (N) provided by both turbofan engine
+Do=1.225;//density(Kg/m^3) at sea level
+D=0.6107;//density(Kg/m^3) at height 6705.6 m
+b=16.25;//wingspan(meter)
+S=29.54;//wingarea(m^2)
+AR=b^2/S;//aspect ratio
+W=88176.75;//normal gross weight(N)
+Cdo=0.02;//parasite drag coefficient
+e=0.81;//oswald efficiency factor
+//in order to find max. velocity we need to find out the intersection of power required curve for example 6.3b and power available curve at height of 6705m:
+
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