Admissions in india 2015
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Transcript of Admissions in india 2015
Admissions in India 2015By:Admission.edhole.com
Measurement of flow rate, friction Factor, and velocity Profile in Pipe Flow
57:020 mechanics of Fluids and Transfer Processes
Experimental Laboratory #2
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Purpose
Measure Flow rate in a pipe (smooth)Friction factorVelocity profileSpecify the turbulent-flow Reynolds NumberCompare the results with benchmark dataUncertainty analysis for:
Friction factor Velocity profile
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Test Design
The facility consists of:Closed pipe networkFanReservoir Instruments used:3 Venturi meters
Simple water ManometerDifferential Water manometerPitot ProbeDigital Micrometer (Accurate radial positioning)
Contraction Diameters (mm):
12.7 25.4 52.93
Flow Coefficient, K 0.915 0.937
0.935
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Air Flow Pipe facility
Pressuretaps
M otorcontro lle r
F loor
6’-6
”
Res
ervo
ir
2.0” sm ooth
0.5” sm ooth2.0” rough
R elie fva lves
B low er
D = 2 .0” D = 1.0”D = 0.5”
tt
t
36’
Venturi m eter gate valvesTherm om eter
1 2 3 4
Valve m anifold
S im plem anom eter
P itot tubehousings
Valves
Differentia lm anom eter
Venturi m eters
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Test Design (Continue)Reservoir:
To build up pressure and force the air to flow downstream through any of the three straight experiment pipes.
Digital Micrometer:Allow the measurement of the position
of the Pitot probe at different locations along the cross section of the pipe tested
Pitot Probe:Located in the glass-wall boxUsed to measure the Stagnation
pressure and calculate the velocity profile in pipe
Venturi meters:Located on each pipe typeUsed to measure flow rate Q along the
differential water manometer
Pressure Taps:Located along each pipe, they are
connected to the simple water manometer to evaluate the head measurement
They are used to calculate the friction factor
Manometers:To measure the head at each pressure
Tap along the pipe and to make the Pitot-tube measurements (simple Manometer)
To measure head drops across the venturi meters (differential Manometer) Admission.edhole.com
Pressure tap manifold and Pitot-tube housing
Pressure tap manifold Pitot-tube housing
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Measurement Systems:
The equipment used in the experiment includes:Digital thermometer with a range of – 40 to 450 F and a smallest reading of 0.1 F for measurement of the environment temperature. Digital micrometer with least significant digit 0.01 mm for positioning the Pitot-tube inside the pipe. Simple water manometer with a range of 2.5 ft and a least scale division of 0.001 ft for measurement of the head at each pressure tap along the pipes and for measurement of velocities using the Pitot-tube arrangement . Differential water manometer with a range 3 ft and a least scale division of 0.001ft for measurement of the head drop across the Venturi meters.
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Measurement Systems (continue)
For the flow rate and friction factor, the individual measurement are performed for:
Ambient air temperature (A.3) Pipe air temperature (A.5) Pipe pressure head Venturi meter pressure head drop
The experimental Results are: Manometer water density Air density Kinematic viscosity Flow rate Reynolds number Friction factor
Data reduction equations are: )( o
ww Tf)( o
airair Tf )( oairair Tf
air
wDMt ZgKAQ
2
aire D
QR
4
ji SMSM
air
w ZZLQDgf
2
52
8
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Measurement Systems (continue)
For the velocity profile, the individual measurement systems are for:
the ambient temperature pipe air temperature pitot stagnation and static pressure heads.
The experimental results are for: manometer water density (A.3) Air density (A.5) Velocity profile (below)
Data reduction equation: (using the Bernoulli equation along the manometer equation)
staticstag SMSMa
w ZrZgru )(2)(
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Flow rate, Friction factor and velocity profile measurement systems
Block diagram of the experimental determination of the Friction
Block diagram of the Velocity measurement
EXPERIMENTALRESULTS
EXPERIMENTAL ERROR SOURCES
INDIVIDUALMEASUREMENT
SYSTEMS
MEASUREMENTOF INDIVIDUAL
VARIABLES
DATA REDUCTIONEQUATIONS
TEMPERATUREWATER
TEMPERATUREAIR
fB , P
VENTURIPRESSURE
PIPEPRESSURE
f = F( , , z , Q = )a a
wg D
8LQ
Q = F( z )
w
w
T
TB T, Pz
zB , P
f f
SM
SMww
DM
SM
2
2
5
aT
TB T, Paa z SM
z
zB , PDM
DM z DM
= F(T )
( )
w
= F(T )a
zSM i
- zSM j
w
a
EXPERIMENTALRESULT
w
w
T
TB T, P
STAGNATIONPRESSURE
STATICPRESSURE
EXPERIMENTAL ERROR SOURCES
INDIVIDUALMEASUREMENT
SYSTEMS
MEASUREMENTOF INDIVIDUAL
VARIABLES
DATA REDUCTIONEQUATIONS
z
B , PSM
B , Pu u
u
= F(T )
u = F( , , z , z ) 2( ) g
½=
TEMPERATUREWATER
TEMPERATUREAIR
w
a stag
a
T
TB T, Pa z
w
ww
SMstag
z SMstag
z
B , PSM stat
zSMstat
z SMstat
= F(T )a
aa SMstag SM stat
zSM stag
- zSM stat
w
a
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Data Acquisition and reduction The procedures for data acquisition and reduction are described as follow:
1. Use the appropriate Venturi meter, (2” smooth pipe) measure the head drop
2. Take reading for ambient air (manometer water) and pipe air temperatures.
3. To obtain velocity data, measure in the appropriate Pitot-tube box, the ambient head and stagnation heads across the full diameter. Measure the stagnation heads at radial intervals. The recommended radial spacing for one half of the diameter is 0, 5, 10, 15, 20, 23, and 24 mm.
4. Maintaining the discharge, measure the head along the pipe by means of the simple water manometer connected to the pressure taps located along the pipe being studied (10 times for uncertainty analysis)
5. Repeat step 26. Execute data reduction for data analysis and uncertainty analysis using
equation above
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Uncertainty AnalysisThe data reduction equation for the friction factor is:
However here we will only consider bias limits for ZSM i and ZSM j . The total uncertainty for the friction is:
The Bias Limit, Bf and the precision limit, Pf, for the result are given by:
),,,,,,,(ji SMSMaw ZZQLDgFf
222fff PBU
2222
1
222
jSMSMjiSMiSM ZZZZ
j
iiif BBBB
M
tSP ff
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Uncertainty Analysis (continue)
Data Reduction equation for the velocity profile is as follow:
222uuu PBU
2222
1
222
statSMstatSMSMstagnstagnSM ZZZZ
j
iiiu BBBB
MtSP u
u
),,,,(staticstagnation SMSMaw ZZgFf
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Moody Chart for pipe friction with smooth and rough walls
10 104
10 10 10 105 6 7 83
0 .0 080 .0 09
0 .0 15
0 .0 25
0 .0 20
0 .010
0 .0 30
0 .0 40
0 .0 50
0 .0 60
0 .0 70
0 .0 800 .0 90
0 .1 0
R eynolds Number, R e = VD
Fric
tion
Fact
or f
=h
f
(L/D
)V /
(2g)
2
0 .00001
0 .00005
0 .0001
0 .0002
0 .00040 .00060 .00080 .001
0 .050 .040 .03
0 .02
0 .01
0 .015
0 .0080 .0060 .004
0 .002
Rel
ativ
e R
ough
ness
, /D
Lam inarF low
Critica lZ one
T ra ns itionZ one
Laminar Flow
f = 64/Re
/D = 0 .0 00005
/D = 0 .000001
Com p le te T urbu lence , Hyd rau lica l ly Rou gh
Hyd rau lica lly S m oo th
k
k
k
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