What is the minimum pump head ( H p ) required by the system in [ ft ] to initiate flow at point "3" in the piping system above?
P r o b l e m I n f o r m a t i o n :
Conservation of Energy derived flow model applied between points "a" and "b" in the system:
ρ g P a + z a + α 2 g v a 2 + H p = ρ g P b + z b + α 2 g v b 2 + ∑ h l a − b
P 0 = P 2 = P 3 = 0 gage ( Ambient Pressure at points 0, 2 & 3, respectively)
z 1 = z 2 = 1 0 [ ft ] (Static Elevation)
z 3 = 5 0 . 5 [ ft ] (Static Elevation)
D 1 = 1 . 5 [ in ] (Interior Pipe Diameter - Section "0 to 1")
D 2 = D 3 = 1 [ in ] ( Interior Pipe Diameter - Sections "1 to 2" & "1 to 3", respectively)
K 0 − 1 = 5 ( Effective Loss Coefficient - Section "0 to 1")
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 ), 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 ] = 2 g K a − b v a − b 2
where,
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 is the average velocity of that flow for a given pipe diameter D i .
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Applying Conservation of Energy in a suitable form for fluids systems (Energy per unit Weight):
S e c t i o n 0 - 1
γ P 0 + z 0 + α 2 g v 0 2 + H p = γ P 1 + z 1 + α 2 g v 1 2 + ∑ 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 : P 0 = 0 gage , z 0 = 0 , v 0 ≈ 0 , α = 1
H p = γ P 1 + z 1 + 2 g v 1 2 + K 0 − 1 2 g v 1 2 ...EQ1
S e c t i o n 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 . A goal is to eliminate γ P 1 from EQ1, solving for it:
γ P 1 = 2 g v 2 2 ( 1 + K 0 − 1 ) − 2 g v 1 2 ...EQ2
S e c t i o n 1 - 3
Same application as above between points 1 and 3 with, H p = 0 , P 3 = 0 gage and the criteria v 3 = 0 , we find:
γ P 1 = ( z 3 − z 1 ) − 2 g v 1 2 ...EQ3
Now we can substite EQ3 into EQ1, eliminating γ P 1 and simplify, finding:
H p = z 3 + K 0 − 1 2 g v 1 2 ...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 :
Q 1 = v 1 A 1 ...EQ4
Rearrange EQ4 for v 1 and sub into EQ1':
H p = z 3 + K 0 − 1 A 1 2 2 g Q 1 2 ...EQ1''
Furthermore, we may apply continuity ( conservation of mass for incompressible flows) at point 1:
Q 1 = Q 2 + Q 3 ...EQ5
Letting Q 3 go to zero:
Q 1 = Q 2
It then follows that:
H p = z 3 + K 0 − 1 A 1 2 2 g Q 2 2 ...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 . ( v 3 = 0 already being accounted for in EQ3) we obtain ( solving for Q 2 2 in terms of v 2 , A 2 ) :
2 g v 2 2 ( 1 + K 0 − 1 ) − 2 g v 1 2 = ( z 3 − z 1 ) − 2 g v 1 2
→ Q 2 2 = 2 g A 2 2 1 + K 1 − 2 z 3 − z 1 ...EQ6
Finally, sub EQ6 into EQ1''', with A 1 A 2 = ( D 1 D 2 ) 2 :
H p = z 3 + 1 + K 1 − 2 K 0 − 1 ( D 1 D 2 ) 4 ( z 3 − z 1 ) = 5 0 . 5 [ ft ] + 1 + 3 5 ( 1 . 5 [ in ] 1 [ in ] ) 4 ( 5 0 . 5 [ ft ] − 1 0 [ ft ] ) = 6 0 . 5 [ ft ]
**Given a pump that outputs the required head, the system flow can be found from EQ6 to be approximately 6 2 . 5 [ gpm ] . Any further increase in head delivered by the pump and the criterion v 3 = 0 no longer holds. To determine head and flow state beyong H p a solution to a system of non-linear equations must be employed ( methods typically involve linearization and iteration)