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Diffstat (limited to '1226/CH12/EX12.2')
-rwxr-xr-x | 1226/CH12/EX12.2/EX12_2.jpg | bin | 0 -> 88529 bytes | |||
-rwxr-xr-x | 1226/CH12/EX12.2/EX12_2.sce | 19 |
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diff --git a/1226/CH12/EX12.2/EX12_2.jpg b/1226/CH12/EX12.2/EX12_2.jpg Binary files differnew file mode 100755 index 000000000..55168e1a4 --- /dev/null +++ b/1226/CH12/EX12.2/EX12_2.jpg diff --git a/1226/CH12/EX12.2/EX12_2.sce b/1226/CH12/EX12.2/EX12_2.sce new file mode 100755 index 000000000..b1e7e2140 --- /dev/null +++ b/1226/CH12/EX12.2/EX12_2.sce @@ -0,0 +1,19 @@ +clc;funcprot(0);//EXAMPLE 12.2
+// Initialisation of Variables
+n=6;...............//No of cylinders
+N=1500;............//Engine rpm
+BP=220;.............//Brake Power in kW
+bsfc=0.273;..........//Brake Specific Fuel Consumption in kg/kWh
+theta=30;.............//The Period of Injection in degrees of crank angle
+spgr=0.85;............//Specific Gravity of fuel
+Cf=0.9;................//Orifice discharge co-efficient
+ip=160;...............//Injection pressure in bar
+cp=40;.................//Pressure in combustion chamber in bar
+rhow=1000;................//Density of water in kg/m^3
+//Calculations
+vf = Cf*sqrt((2*(ip-cp)*10^5)/(spgr*rhow));.............//Actual fuel velocity of injection in m/sec
+qf=(bsfc*BP)/(spgr*rhow*3600);..................// Volume of fuel injected per sec in m^3
+d=sqrt (qf/((%pi/4)*n*vf*(theta/360)*(60/N)*(N/120)));...........//Diameter of nozzle orifice
+disp(d,"Diameter of Nozzle Orifice is (m):")
+
+
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