• System sketch: Figure E3.24 shows the proper selection for sections 1 and 2.
• Assumptions: Steady flow, negligible viscous work, large reservoir (V_1 ≈ 0).
• Approach: First find the velocity V_2 at the exit, then apply the steady flow energy equation.
• Solution steps: Use BG units, p_1 = 14.7(144) = 2117 lbf/ft^2 and p_2 = 10(144) = 1440 lbf/ft^2.
Find V_2 from the known flow rate and the pipe diameter:
V_2 = \frac{Q}{A_2} = \frac{1.5 ft^3/s}{(\pi/4)(3/12 ft)^2} = 30.6 ft/s
The steady flow energy equation (3.75), with a pump (no turbine) plus z_1 ≈ 0 and V_1 ≈ 0, becomes as shown in Figure 3.24a or:
h_p = \frac{p_2 – p_1}{\gamma} + z_2 + (\alpha_2 + K) \frac{V_2^2}{2g}
\left(\frac{p}{\rho g} + \frac{\alpha}{2g} V^2 + z\right)_{in} = \left(\frac{p}{\rho g} + \frac{\alpha}{2g} V^2 + z\right)_{out} + h_{turbine} – h_{pump} + h_{friction} (3.75)
• Comment: The pump must balance four different effects: the pressure change, the elevation change, the exit jet kinetic energy, and the friction losses.
• Final solution: For the given data, we can evaluate the required pump head:
h_p = \frac{(1440 – 2117) lbf/ft^2}{62.4 lbf/ft^3} + 20 + (1.07 + 7.5) \frac{(30.6 ft/s)^2}{2(32.2 ft/s^2)} = -11 + 20 + 124 = 133 ft
With the pump head known, the delivered pump power is computed similar to the turbine in Example 3.23:
P_{pump} = \dot{m}w_s = \gamma Qh_p = \left(62.4\frac{lbf}{ft^3}\right) \left(1.5\frac{ft^3}{s}\right) (133 ft) = 12450 \frac{ft – lbf}{s} = \frac{12,450 ft-lbf/s}{550 ft-lbf/(s-hp)} = 22.6 hp
If the pump is 80 percent efficient, then we divide by the efficiency to find the input power required:
P_{input} = \frac{P_{pump}}{efficiency} = \frac{22.6 hp}{0.80} = 28.3 hp
• Comment: The inclusion of the kinetic energy correction factor α in this case made a difference of about 1 percent in the result. The friction loss, not the exit jet, was the dominant parameter.