10.55: PROBLEM DEFINITION
Situation:
Water is draining out of a tank through a galvanized iron pipe.
ks=0.006 in = 5 ×104ft,L=10ft,H=4ft.
Thepipeis1inschedule40NPS,D=1.049 in = 0.08742 ft.
Find:
Velocity in the pipe (ft/s).
Flow rate (cfs)
Assumptions:
Steady ow.
Component head loss is zero.
Turbulent ow. Also, α2=1.0.
Properties:
Water (70 F), Table A.5, ρ=1.94 slug/ft3=62.3lbf/ft3,ν=1.06 ×105ft2/s.
PLAN Classify this problem as case 2 (Vis unknown), then
1. Write the energy eqn., the Darcy-Weisbach eqn., etc. to produce a set of 4
equations with 4 unknowns.
3. Find the ow rate with Q=VA.
SOLUTION
1. Governing equations:
Energy equation (section 1 on water surface, section 2 at exit plane)
Darcy-Weisbach:
81
2. Solution of Eqs. (1) to (4):
3. Flow rate equation:
REVIEW
Notice that the turbulent ow assumption is valid because Re >2300.
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10.56: PROBLEM DEFINITION
Situation:
Water is draining out of a tank through a galvanized iron pipe.
L=2m,H=1m,ks=0.15 ×103m
Thepipeis0.5inschedule40NPS,D=0.622 in = 0.0158 m.
Find:
Velocity in the pipe (ft/s).
Assumptions:
Steady ow.
Component head loss is zero.
Turbulent ow, so α2=1.0.
Properties:
Water (15 C), Table A.5, ν=1.14 ×106m2/s.
PLAN
Classify this problem as case 2 (Vis unknown), then
1. Write the energy eqn., the Darcy-Weisbach eqn., etc. to produce a set of 4
SOLUTION
1. Governing equations:
Energy equation (section 1 on water surface, section 2 at exit plane)
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3. Solution of Eqs. (1) to (4):
REVIEW
1. Notice that the turbulent ow assumption is valid because Re >2300.
2. An easy way to solve case 2 and case 3 problems is to acquire a computer program
10.57: PROBLEM DEFINITION
Situation:
Air is owing in a horizontal copper tube.
L=150m,Q=0.1m
3/s,ks=1.5×106m.
Pressure drop in the tube cannot exceed p=6in-H20 = 1493 Pa.
Find:
Tube diameter (meters).
Assumptions:
Steady ow. Fully developed ow.
Component head loss is zero.
Turbulent ow.
Properties:
Air (40 C,1atm),TableA.5,γ=11.1N/m3=1.69 ×105m2/s.
PLAN
Classify this problem as case 3 (Dis unknown), then
1. Write the energy eqn., the Darcy-Weisbach eqn., etc. to produce a set of 5
equations with 5 unknowns.
2. Solve the set of equations using a computer program (we used TK Solver).
SOLUTION
1. Governing equations:
Flow rate equation:
Energy equation (section 1 is located 150 m upstream from section 2).
Darcy-Weisbach:
85
3. Solution of Eqs. (1) to (5):
REVIEW . The turbulent ow assumption is valid because Re >2300.
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10.58: PROBLEM DEFINITION
Situation:
Auid ows through a galvanized iron pipe.
D=8cm.
Pipe slope is 1 Horizontal to 10 Vertical.
Sketch:
Find:
Flow rate.
Properties:
From Table 10.4 ks=0.15 mm.
ρ=800kg/m3,ν=10
6m2/s.
SOLUTION
Energy equation
Relative roughness
Resistance coecient. From Fig. 10.14 (in 10e) f=0.025.Then
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10.59: PROBLEM DEFINITION
Situation:
Commercial steel pipe will convey water.
hL=1 ft per 1000 ft of pipe length.
Q=300ft
3/s.
Find:
Pipe diameter to produce specied head loss.
Assumptions:
The pipes are available in even inch sizes (e.g. 10 in., 12 in., 14 in., etc.)
Properties:
Water (60 F), Table A.5: ν=1.22 ×105ft2/s.
From Table 10.4: ks=0.002 in = 1.7×104ft.
SOLUTION
Darcy Weisbach equation
2hf1/5
Assume f=0.015
Now get a better estimate of f:
Compute Dagain:
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10.60: PROBLEM DEFINITION
Situation:
A steel pipe will carry crude oil.
Q=0.1m
3/s.
hL=50mper km of pipe length.
Find:
(a) Diameter of pipe for a head loss of 50 m.
(b) Pump power.
Assumptions:
Available pipe diameters are D=20,22,and 24 cm.
Properties:
From Table 10.4: ks=0.046 mm.
S=0.93,ν=10
5m2/s.
SOLUTION
Darcy Weisbach equation
Assume f=0.015
91
Calculateamoreaccuratevalueoff
Recalculate diameter using new value of f
Power equation (assume the head loss is remains at hL50 m/1,000 m)
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10.61: PROBLEM DEFINITION
Find:
Use Table 10.5 (in §10.8) to select loss coecients, K, for the following transitions
and ttings.
a. A threaded pipe 90elbow.
b. A 90smooth bend with r/d =2.
c. A pipe entrance with r/d of 0.3.
d. An abrupt contraction, with θ=180
,andD2/D1=0.60.
e. A gate valve, wide open.
SOLUTION
a. Answer: 0.9
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10.62: PROBLEM DEFINITION
Situation:
An electrostatic air lter is being tested.
Pressure drop is p=3in.H
20. Air speed is V=10m/s.
Find: The minor loss coecient (K)for the lter.
Properties:
Air (20 C) Table A.3: ν=15.1×106m2/s.
ρ=1.2kg/m3,γ=11.8N/m3.
PLAN
Apply the energy equation to relate the pressure drop to head loss. Then, nd the
minor loss coecient using hL=KV 2/2g.
SOLUTION
Energy equation (select a control volume surrounding the lter)
94
Head loss
K=12.4(2)
REVIEW
2.) Combining Eqs. (1) and (2) gives K=p/(ρV 2/2).Thus, the pressure drop for
the lter is about 12 times larger that the pressure change that results when the ow
is brought to rest.
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10.63: PROBLEM DEFINITION
Situation:
Water is pumped between reservoirs through a steel pipe.
Q=0.1m
3/s,D=15cm.
Sketch:
Find:
Power that is supplied to the system by the pump.
Properties:
From Table 10.4: ks=0.046 mm.
Water (10 C),TableA.5: v=1.3×106m2/s,γ=9810N/m3.
SOLUTION
Flow rate equation
Reynolds number
Resistance coecient (from the Moody diagram, Fig. 10.14 in EFM10e)
Energy equation (between the reservoir surfaces)
Power equation
97
10.64: PROBLEM DEFINITION
Situation:
A siphon tube is used to drain water from a jug into a graduated cylinder.
Dtube =3/16 in. =0.01562 ft.
Ltube =50in,V=500ml.
Sketch:
Find:
Time to ll cylinder.
Assumptions:
T60oFwithν=1.2×105ft2/s.
Neglect head loss associated with any bend in the Tygon tube.
SOLUTION
Energy equation (from the surface of the water in the jug to the surface in the
graduated cylinder)
Assume that the entrance loss coecient is equal to 0.5. It could be larger than 0.5,
but this should yield a reasonable approximation. Therefore
Theexitlosscoecient, KE, is equal to 1.0. Therefore, Eq. 1 becomes
98
Resistance coecient (recalculate)
Repeat calculations with a new value of friction factor.
Use f=0.040 for nal solution. As a simplifying assumption assume that as the
cylinder lls the level of water in the jug has negligible change. As the cylinder is
Substitute Vof Eq. (1) into Eq. (2):
or
The dierential equation becomes
Let hbe measured from the level where the cylinder is 2 in full. Then
Now we have
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