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+clc;funcprot(0);//EXAMPLE 16.2
+// Initialisation of Variables
+p1=1.0132;..............//Mean pressure at sea level in bar
+t1=283;................//Mean temperature at sea level in Kelvin
+BP=260;....................//Brake Power output in kW
+etaV=0.78;..................//Volumetric efficiency at sea level free air condition
+sfc=0.247;............//Specific Fuel consumption in kg/kW.h
+afr=17;...................//Air fuel ratio
+N=1500;...................//Engine rpm
+at=2700;.................//Altitude in mts
+p2=0.72;................//Pressure in bar at the given altitude
+Psup=0.08;.................//8% power of engine is taken by the supercharger
+R=287;...................//Gas constant in J/kgK
+t2=32+273;..............//Temperature in Kelvin at the given altitude
+//calculations
+mf=(sfc*BP)/60;.............//Fuel consumption in kg/min
+ma = mf*afr;..................//Air consumption in ig/min
+acps = ma/(N/2);............//Air consumption per stroke in kg
+Vs=(acps*R*t1)/(etaV*p1*10^5);................//Engine capacity in m^3
+disp(Vs,"The Engin Capacity in m^3:")
+pmb=(BP*6)/(Vs*10*(N/2));........//Brake Mean Effective Pressure in bar
+disp(pmb,"The Brake mean effective pressure is (bar) :")
+gp=BP/(1-Psup);.................//Gross power produced by supercharged engine in kW
+masup=ma*gp/BP;......................//Mass of air required for supercharged engine in kg
+matc=masup/(N/2);..............//Mass of air taken per cycle
+pressure=(matc*R*t2)/(etaV*10^5*Vs);
+disp(pressure-p2,"The Increase of pressure required (in bar):")