To Pump or Not to Pump?

What is the minimum pump head ( H p H_p ) required by the system in [ ft ] [\text{ft}] to initiate flow at point "3" in the piping system above?

Problem Information: \textbf{\underline{Problem Information:}}

Conservation of Energy derived flow model applied between points "a" and "b" in the system:

P a ρ g + z a + α v a 2 2 g + H p = P b ρ g + z b + α v b 2 2 g + h l a b \displaystyle \frac{P_a}{\rho g} + z_a + \alpha \frac{{v_a}^2}{2g} + H_p = \frac{P_b}{\rho g} + z_b + \alpha \frac{{v_b}^2}{2g} + \sum{h_{l_{a-b}}}

P 0 = P 2 = P 3 = 0 gage P_0 = P_2 = P_3 = 0 \, \text{gage} ( Ambient Pressure at points 0, 2 & 3, respectively)

z 1 = z 2 = 10 [ ft ] z_1 = z_2 = 10 \,[\text{ft}] (Static Elevation)

z 3 = 50.5 [ ft ] z_3 = 50.5 \, [\text{ft}] (Static Elevation)

D 1 = 1.5 [ in ] D_1 = 1.5 \, [\text{in}] (Interior Pipe Diameter - Section "0 to 1")

D 2 = D 3 = 1 [ in ] D_2 = D_3 = 1 \, [\text{in}] ( Interior Pipe Diameter - Sections "1 to 2" & "1 to 3", respectively)

K 0 1 = 5 K_{0-1} = 5 ( Effective Loss Coefficient - Section "0 to 1")

K 1 2 = K 1 3 = 3 K_{1-2} = K_{1-3} = 3 ( Effective Loss Coefficient - Section "1 to 2" & "1 to 3", respectively)

The reservoir is taken to be very large; as such its depth remains approximately constant, and the kinetic head at point "0" is to be neglected.

All flows are assumed incompressible, turbulent (kinetic head correction factor α = 1 \alpha = 1 ), irrotational, and viscous. Thermal losses (head loss for piping and fittings in any portion of the system) are to be modeled as follows:

h l a b [ ft ] = K a b 2 g v a b 2 h_{l_{a-b}}[\text{ft}] = \frac{K_{a-b}}{2g}v_{a-b}^2

where,

K a b K_{a-b} is the effective loss coefficient (taken to be exact) for the transmission of flow between points "a" and "b" in the piping system, and v a b v_{a-b} is the average velocity of that flow for a given pipe diameter D i D_{i} .


The answer is 60.5.

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1 solution

Eric Roberts
Sep 14, 2019

Applying Conservation of Energy in a suitable form for fluids systems (Energy per unit Weight):

Section 0 - 1 \textbf{\underline{Section 0 - 1}}

P 0 γ + z 0 + α v 0 2 2 g + H p = P 1 γ + z 1 + α v 1 2 2 g + h l 0 1 \displaystyle \frac{P_0}{\gamma} + z_0 + \alpha \frac{{v_0}^2}{2g} + H_p = \frac{P_1}{\gamma} + z_1 + \alpha \frac{{v_1}^2}{2g} + \sum{h_{l_{0-1}}}

Begin by simplifying the expression and substitute in the relation for head loss in the problem statement, solve for H p H_p : P 0 = 0 gage , z 0 = 0 , v 0 0 , α = 1 P_0 = 0 \, \text{gage}, z_0 = 0, v_0 \approx 0, \alpha =1

H p = P 1 γ + z 1 + v 1 2 2 g + K 0 1 v 1 2 2 g \displaystyle H_p = \frac{P_1}{\gamma} + z_1 + \frac{{v_1}^2}{2g} + K_{0-1}\frac{{v_1}^2}{2g} ...EQ1

Section 1 - 2 \textbf{\underline{Section 1 - 2}}

This is the same analysis as above applied between points 1 and 2 with: H p = 0 , z 1 = z 2 , P 2 = 0 gage H_p = 0, z_1 = z_2, P_2 = 0 \, \text{gage} . A goal is to eliminate P 1 γ \frac{P_1}{\gamma} from EQ1, solving for it:

P 1 γ = v 2 2 2 g ( 1 + K 0 1 ) v 1 2 2 g \displaystyle \frac{P_1}{\gamma} = \frac{{v_2}^2}{2g}(1 + K_{0-1}) - \frac{{v_1}^2}{2g} ...EQ2

Section 1 - 3 \textbf{\underline{Section 1 - 3}}

Same application as above between points 1 and 3 with, H p = 0 , P 3 = 0 gage H_p = 0, P_3 = 0 \, \text{gage} and the criteria v 3 = 0 v_3 = 0 , we find:

P 1 γ = ( z 3 z 1 ) v 1 2 2 g \displaystyle \frac{P_1}{\gamma} = (z_3 - z_1) - \frac{{v_1}^2}{2g} ...EQ3

Now we can substite EQ3 into EQ1, eliminating P 1 γ \frac{P_1}{\gamma} and simplify, finding:

H p = z 3 + K 0 1 v 1 2 2 g H_p = z_3 + K_{0-1}\frac{{v_1}^2}{2g} ...EQ1'

Assuming the velocity profile is approximately constant across the pipes, we can derrive the velocity of the flow in terms of the volumetric flow rate using the cross sectional area A 1 A_1 :

Q 1 = v 1 A 1 \displaystyle Q_1 = v_1A_1 ...EQ4

Rearrange EQ4 for v 1 v_1 and sub into EQ1':

H p = z 3 + K 0 1 Q 1 2 A 1 2 2 g \displaystyle H_p = z_3 + K_{0-1}\frac{{Q_1}^2}{{A_1}^2 2g} ...EQ1''

Furthermore, we may apply continuity ( conservation of mass for incompressible flows) at point 1:

Q 1 = Q 2 + Q 3 \displaystyle Q_1 = Q_2 + Q_3 ...EQ5

Letting Q 3 Q_3 go to zero:

Q 1 = Q 2 \displaystyle Q_1 = Q_2

It then follows that:

H p = z 3 + K 0 1 Q 2 2 A 1 2 2 g \displaystyle H_p = z_3 + K_{0-1}\frac{{Q_2}^2}{{A_1}^2 2g} ...EQ1'''

Now, since Branch 1-2 & 1-3 are in parallel, they have a common pressure at point 1. We may equate EQ2 and EQ3 through the common pressure P 1 P_1 . ( v 3 = 0 v_3 = 0 already being accounted for in EQ3) we obtain ( solving for Q 2 2 {Q_2}^2 in terms of v 2 , A 2 v_2, A_2 ) :

v 2 2 2 g ( 1 + K 0 1 ) v 1 2 2 g = ( z 3 z 1 ) v 1 2 2 g \displaystyle \frac{{v_2}^2}{2g}(1 + K_{0-1}) - \frac{{v_1}^2}{2g} = (z_3 - z_1) - \frac{{v_1}^2}{2g}

Q 2 2 = 2 g A 2 2 z 3 z 1 1 + K 1 2 \displaystyle \rightarrow {Q_2}^2 = 2g{A_2}^2\frac{z_3-z_1}{1+K_{1-2}} ...EQ6

Finally, sub EQ6 into EQ1''', with A 2 A 1 = ( D 2 D 1 ) 2 \frac{A_2}{A_1} = \left( \frac{D_2}{D_1} \right)^2 :

H p = z 3 + K 0 1 1 + K 1 2 ( D 2 D 1 ) 4 ( z 3 z 1 ) = 50.5 [ ft ] + 5 1 + 3 ( 1 [ in ] 1.5 [ in ] ) 4 ( 50.5 [ ft ] 10 [ ft ] ) = 60.5 [ ft ] \displaystyle H_p = z_3 + \frac{K_{0-1}}{1+K_{1-2}}\left(\frac{D_2}{D_1}\right)^4(z_3 - z_1) = 50.5 \, [\text{ft}] + \frac{5}{1+3}\left(\frac{1 \, [\text{in}]}{1.5\, [\text{in}]}\right)^4 (50.5 \, [\text{ft}] - 10 \, [\text{ft}]) = 60.5 \, [\text{ft}]

**Given a pump that outputs the required head, the system flow can be found from EQ6 to be approximately 62.5 [ gpm ] 62.5 \, [\text{gpm}] . Any further increase in head delivered by the pump and the criterion v 3 = 0 v_3 = 0 no longer holds. To determine head and flow state beyong H p H_p a solution to a system of non-linear equations must be employed ( methods typically involve linearization and iteration)

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