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authorpriyanka2015-06-24 15:03:17 +0530
committerpriyanka2015-06-24 15:03:17 +0530
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+//mass of air flow(in kg/min)
+ma=5;
+//mass of fuel flow(in kg/min)
+mf=0.5;
+//specific gravity of fuel
+Pf=0.75;
+//pressure of air at inlet(in bar)
+p1=1;
+//temperature at inlet(in K)
+T1=300;
+//velocity coefficient
+Vc=0.8;
+//ratio of pressure drop of metering orifice to choke
+pd=0.8;
+//specific heat a constant pressure
+Cp=1005;
+//gas constant
+R=0.287;
+//coefficient of discharge of fuel
+Cf=0.6;
+//adiabatic constant
+y=1.4;
+//velocity at throat(in m/s)
+C2=100; \ No newline at end of file