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Diffstat (limited to '1226/CH11/EX11.1')
| -rwxr-xr-x | 1226/CH11/EX11.1/EX11_1.jpg | bin | 0 -> 87768 bytes | |||
| -rwxr-xr-x | 1226/CH11/EX11.1/EX11_1.sce | 17 |
2 files changed, 17 insertions, 0 deletions
diff --git a/1226/CH11/EX11.1/EX11_1.jpg b/1226/CH11/EX11.1/EX11_1.jpg Binary files differnew file mode 100755 index 000000000..f1cf16af0 --- /dev/null +++ b/1226/CH11/EX11.1/EX11_1.jpg diff --git a/1226/CH11/EX11.1/EX11_1.sce b/1226/CH11/EX11.1/EX11_1.sce new file mode 100755 index 000000000..f9a178053 --- /dev/null +++ b/1226/CH11/EX11.1/EX11_1.sce @@ -0,0 +1,17 @@ +clc;funcprot(0);//EXAMPLE 11.1
+// Initialisation of Variables
+d=0.1;..................//Cylinder bore in m
+l=0.12;................//Cylinder stroke in m
+N=1800;..................//Engine rpm
+d2=0.028;................//Throat diameter in m
+Cda=0.8;................//Co efficient of air flow
+etaV=0.75;..................//Volumetric efficiency
+rhoa=1.2;................//Density of air in kg/m^3
+n=4;.......................//No of cylinders
+//Calculations
+Vs=(%pi/4)*d*d*l*n;.................//Stroke Volume in m^3
+Va=etaV*Vs;.......................//Actual volume per stroke in m^3
+Vas=Va*(N/2)*(1/60);.............//Actual volume sucked per second
+ma=Vas*rhoa;.........................//Air consumed in kg/sec
+delp=((ma/(Cda*(%pi/4)*d2*d2))^2)/(2*rhoa);.............//Suction at throat in N/m^2
+disp(delp,"Suction at throat (in N/m^2):")
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