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authorpriyanka2015-06-24 15:03:17 +0530
committerpriyanka2015-06-24 15:03:17 +0530
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+//for the cessna skylane(CP-1):
+W=11494.35;//fuel empty weight(N)
+W1=3916//total weight(N) including pilot seat etc
+Wf=1633.15;//weight(N) of fuel
+Wo=W+Wf-W1 //gross weight of UAV
+b=10.912;//wingspan(meter)
+S=16.16;//wingarea(m^2)
+AR=b^2/S//aspect ratio
+D=1.225;//density at sea level(Kg/m^3)
+Cdo=0.025;//parasite drag coefficient
+e=0.8;//oswald efficiency factor
+Pa=0.8*230*746 //maximum power available(J/s) from example 6.4
+//from example 6.12:
+n=0.8;
+c=7.45*10^-7;