diff options
Diffstat (limited to '2223/CH18/EX18.4/Ex18_4.sce')
-rwxr-xr-x | 2223/CH18/EX18.4/Ex18_4.sce | 29 |
1 files changed, 29 insertions, 0 deletions
diff --git a/2223/CH18/EX18.4/Ex18_4.sce b/2223/CH18/EX18.4/Ex18_4.sce new file mode 100755 index 000000000..8e55e700d --- /dev/null +++ b/2223/CH18/EX18.4/Ex18_4.sce @@ -0,0 +1,29 @@ +// scilab Code Exa 18.4 Calculation on a Diffuser
+
+pe=35; // Initial Pressure in mm W.G.
+pa=1.0135; // ambient pressure in bar
+c1=100; // entry velocity in m/s
+C_pa=0.602; // actual pressure recovery coefficient
+ro=1.25; // density in kg/m3
+g=9.81; // Gravitational acceleration in m/s^2
+Ar=1.85; // Area Ratio of Diffuser
+
+// part(a)
+C_ps=1-(1/(Ar^2));
+disp(C_ps,"(a)ideal value of the pressure recovery coefficient is")
+
+// part(b)
+n_D=C_pa/C_ps;
+disp ("%",n_D*1e2,"(b)Efficiency of the diffuser is")
+
+// part(c)
+p1=pa+(pe*g*1e-5);
+p01=p1+(0.5*ro*(c1^2)*1e-5);
+delp_0=(C_ps-C_pa)*(0.5*ro*(c1^2)*1e-5);
+disp("mm W.G.",delp_0*1e5/g,"(c)the stagnation pressure loss across the diffuser is")
+
+// part(d)
+p02=p01-delp_0;
+c2=c1/Ar;
+p2=p02-(0.5*ro*(c2^2)*1e-5);
+disp("mm W.G.",(p2-pa)*1e5/g,"(d)the gauge pressure at the diffuser exit is")
|