Recalculate the maximum Mach number at the impeller eye for the same data as in the previous question, assuming prewhirl angle of 20°.
Figure 4.16 shows the velocity triangle with the prewhirl angle.
From the velocity triangle:
C_1 = \frac{145} {\cos(20°)} = 154.305 m/s
Equivalent dynamic temperature:
\frac{C^2 _1} {2C_p} = \frac{154.305^2}{(2)(1005)} = 11.846 K
C_{w1} = \tan(20°) C_{a1} = (0.36)(145) = 52.78 m/s
Relative velocity at the inlet:
V^2_1 = C^2_a + (U_e – C_{w1})^2 = 145² + (220 – 52.78)², or V_1
= 221.3 m/s
Therefore the static temperature at the inlet:
T_1 = T_{01} – \frac{C^2_1} {2C_p} = 290 – 11.846 = 278.2 K
Hence,
M_1 = \frac{V_1}{\sqrt{γRT_1}} = \frac{221.3}{\sqrt{(1.4)(287)(287.2)}} = 0.662
Note the reduction in Mach number due to prewhirl.