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7/23/2019 Chemical Engineering Laboratory 2 John Loro
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[Chemical Engineering Laboratory 2]
SEGi University
EXPERIMENT 1: BERNOULIS PRINCPLE
Candidates Name: J!n Lr Emman"e#
St"dent I$: SCM%&'(()*
Gr"+ Mem,ers Name: Ms!sen M!amad -.ad!
-,da##a Sa#! S"#iman
M!ammad N"mair Naeem
Emad -#%S!adadi
Le/t"rer0 S"+ervisr:
$ate S",missin: 1201&0'&13
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1.0 OBJECTIVE
The objective of this experiment is to invertigate Bernoulli's law and
pressure dispersion along the endeavor tube. The "Bernoulli's
guideline" trial investigates the Bernoulli's legitimacy mathematical
statement by applying it to the stream of water in a decreasing even
tube. This is done to gure out whether the aggregate weight head
stays consistent along the tube's length as anticipated by the
comparison since the Bernoulli's mathematical statement expresses
that varieties in static weight head along the tube can be computed
through the mathematical statement. Toward the test's end,
diagrams of stream speed versus estimation focuses and weight
appropriation along venture tube is readied for both set and set !.
2.0 THEORY/INTRODUCTION
The Bernoullis e#uation simply states that pressure of the same
li#uid at the same level is the same. This theory is applied onto a
simple device to measure the pressure distribution along the
venture tube. $onsider rst a simple device to measure the local
velocity in a %uid stream along the venture tube. &t the same level,
there are several narrow tubes inserted into the venture tube.
riction is negligible along the streamline through the venture tube,
so that the Bernoullis e#uation for the constant head, h(
=+=+
g
VP
g
V
g
P
''
'
''
'
11
constant
This e#uation also states that the pressure head, elevation head and
velocity head are constant along the venture tube. The friction along
the tube is negligible.
&llowance for friction losses and conversion of the pressure, )and
)!into static pressure heads, hand h!yields(
fhg
Vh
g
Vh ++=+
''
'
'
'
'
1
1
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*here, )+ pressure at crosssection, &
h+ pressure head at crosssection, &
-+ %ow velocity at crosssection, &
)!+ pressure at crosssection, &!
h!+ pressure head at crosssection, &!
-!+ %ow velocity at crosssection, &!
+ density of medium
hf+ pressure loss head
igure $onditions in venturi tube with measurement
points
igure ! /ass %ow conditions in venturi tube
The mass %ow is constant in closed systems( m1=m2
0iven, m=V
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V1=V
2
V1=V
2
0iven, - + & 1 w
A1
V1=A
2V
2=constant
or dynamic pressure head(
hdyn=htothstat
igure 2 3eropoint di4erence of 56mm between the pressures
gauges
7f there is a 8eropoint di4erence of 56mm between the
pressures gauges, 56mm must be subtracted(
hdyn=htothstat
The velocity, *meanswas calculated from the dynamic pressure(
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4' dynmea ghV =
3.0 APPARATUS
i. 9/:6.6; Bernoullis Theorem ingle water pressure gauge
c.
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igure = 9/:6.6; Bernoullis theorem demonstration
igure :
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Table $ross >ection &rea
Pint5 i A5 6mm'7 A5 61&%*m'7
338.6 3.386
! 233.5 2.335
2 84.60 0.8460
= 170.2 1.702
: 255.2 2.552
338.6 3.386
4.0 PROCEDURES
. )erform a #uicD inspection to ensure that the unit is in proper
operating condition.
!. /aDe a hose connection and connect the unit to the nearest
power supply.
2. ?pen the discharge pipe.
=. >et the cap nut @A of probe compression gland such that the
slight resistance is felt on moving probe.
:. ?pen inlet and outlet valves.
. >witch on pump and slowly open main cocD.
;. ?pen vent valves @!A on water pressure gauge and carefully
close outlet cocD until pressure gauges are %ushed.
5. By simultaneously setting inlet and outlet cocD, regulate water
level in pressure gauges such that neither upper nor lower
range limit @EF, FFA is overshot or undershot.
G. Hecord pressures at all measurement points. Then, move
overall pressure probe to corresponding measurement level
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and note down overall pressure.
6.
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iA >et
6 ! 2 = : ;
6
:66
666
:66
!666
Flow !"lo#$%& '() *"+,-, ."/,-+"."0% 1o$0%,
*calc.
*means
2"/,-+"."0% 1o$0%,
Flow !"lo#$%&3(
>et !
6 ! 2 = : ;
6
:66
666
:66
!666
Flow !"lo#$%& '() !"+,-, ."/,-+"."0% 1o$0%,
*calc
*means
2"/-+"."0% 1o$0%,
Flow !"lo#$%&3 (
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iiA >et
6 ! 2 = : ;
6
:6
66
:6
!66
!:6
266
2:6
P+",,-+" $,%$-%$o !"+,-, ",-+""% o$%,
9total
9static
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6.0 DISCUSSION
The objectives of this experiment is to investigate the validity of the
Bernoulli e#uation when applied to the steady %ow of water in atapered duct and to measure the %owrates and both static and total
pressure heads in a rigid convergent and divergent tube of Dnown
geometry for a range of steady %ow rates. This experiment is
based on the Bernoullis principle which relates between velocities
with the pressure for an inviscid %ow. or
both set and !, the *means is more than the * calc. The diagram
demonstrates that at point !, the speed increments somewhat.
Between point ! and point 2, there is a huge change in the speed.
rom point 2 to point =, the speed diminishes massively. rom point
= to point : and point , the speed diminishes marginally. rom this
example of stream speed, it is reali8ed that the outcome is because
of the blunder happened amid the analysis. Both
the set and set ! appear to be having the same example of weight
appropriation in which the static weight is con%icting whereby it
increments till point 2 then begins to diminishing till point . or the
dynamic weight, it join upwards at point 2 while downwards for
static weight.
7.0 CONCLUSION
rom this experiment we found out that %uid %owing under
hori8ontal streamline will folows the bernoullis principle where
when the speed of %iud increase, the pressure of the %uid will
decrease. & venturi tube can be used for %ow rate measurements.
7n comparison with orice or no88le, there is afar more smaller
pressure loss durning measurement of %ow rate. The pressure lossbetween largest and smallest diametter of the tube is used as
measure for the %ow rate. The mistaDes happened during the
experiment denitely a4ects the result. The blunder found was the
blocDage of pitot tube, this erro can be adjusted by cleaning the
pitot tube utili8ing an in number and sharp stricD. The outlet is too
low because of this bocDage.
8.0 E!EE"CE#
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1.luid mechanics and hydraulic machines