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