Fluid Measuring System.pdf

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    PERCOBAAN:

    FLUID MEASURING SYSTEM

    1. Tujuan:

    (a) Verifikasi secara experimental anggapan persamaan Bernoulli.

    (b) Mengamati dan mengukur karakter Venturi Meter, Orifice, dan Rotameter.

    2. Theory:

    (a). Bernoulli Equation

    Assume that the following apply:

    Steady flow Incompressible flow Flow along a streamline No frictional forces

    The Bernoulli equation, which expresses the principle of conservation of linear momentum

    under special circumstances, can written as :

    2

    2

    221

    2

    11

    22gz

    VPgz

    VP

    (1)

    In addition, let assume 21 zz . Therefore, we have

    22

    2

    22

    2

    11 VPVP

    (2)

    Let us consider the continuity equation (conservation of mass) and limit it to the same

    assumption as above. Then we have

    2211 AVAV

    where

    4

    21

    1

    DA

    4

    22

    2

    DA (3)

    2

    2

    1

    1

    2

    1

    2

    D

    D

    A

    A

    V

    V (4)

    Solving forP2from equation (2)

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    2

    1

    2

    1

    2

    2

    112

    V

    V

    VPP

    Substituting for V

    2 / V

    1 from equation (4)

    2

    1

    4

    2

    1

    2

    112

    D

    D

    VPP

    Noting that

    11 AVm

    11

    A

    mV

    21

    2

    1A

    mV

    4

    2

    1

    2

    1

    2

    12 12 D

    D

    A

    mPP

    (5)

    orpressure at any locationxis given by

    4

    1

    2

    1

    2

    1 1

    2 xD

    D

    A

    mPxP

    (6)

    or, since

    g

    xPxh

    )()(

    one can write

    4

    1

    2

    1

    2

    2

    1)(

    12

    )(xD

    D

    Ag

    mhxh

    (7)

    Hence the pressure head at any location along the test section can be expressed in term of the

    pressure at a reference location (inlet).

    (b). Venturi meter

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    Assuming that there is no loss of energy along the pipe, and that the velocity and

    piezometric heads are constant across each of the sections considered, then Bernoullis

    theorem states that

    u21

    2g + h1=

    u22

    2g + h2=

    u2n

    2g + hn (8)

    Where u1, u2 and un are the velocities of flow through section 1, 2, and n. The equation of

    continuity is

    u1A1= u2A2= unAn= Q (9)Q denotes the volume flow or discharge rate.

    Substituting in equation (8) for u1 from equation (9)

    u22

    2g

    A2

    A1

    2

    + h1=u2

    2

    2g+ h2 (10)

    And solving this equation for u2 leads to

    u2=

    vuut2g(h1 h2)1

    A2A1

    2

    (11)

    So that the discharge rate, from equation becomes:

    Q = A2vuut2g(h1 h2)

    1 A2A1

    2 (12)

    In practice, there is some loss of energy between sections 1 and 2, and the velocity is not

    constant across either of these sections. Consequently, measured values of Q usually fall

    a little short of those calculated from equation (3) and it is customary to allow for this

    discrepancy by writing:

    Q = CA2

    vuut

    2g(h1 h2)

    1 A2A1

    2 (13)

    C is known as the coefficient of the meter, which may be established by experiment. Its

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    value varies slightly from one meter to another and even for a give meter it may vary

    slightly with the discharge, but usually lies within the range of 0.92 to 0.99.

    (c). Orifice meter

    The governing equation is similar to eq.(13) of the venturi meter, but with different values of

    coefficient and characteristic.

    Q = CAo

    vuut2g(h5 h6)1

    AoA5

    2

    (14)

    3. Gambar alat:

    7

    9

    5 6 7

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    Gambar 1

    Schematic diagram Venturi meter

    Table 1Lokasi Pressure tap locations dan diameters pada lokasi pressure tap

    Pressure location A B C D

    Diameter (mm) 26 16 26

    x (mm) from A 0 46 156

    4. Pengamatan dan perhitungan

    (a) Lakukan percobaan untuk 5 macam flowrate yang berbeda. Isikan pada Tabel 2.

    (b) Buatlah perhitungan teoritis nilaih(x)untuk setiap flowrate dan bandingkan

    dengan hasil percobaan.

    h(x) = h1+ _m2

    22gA21 "1

    D1

    D(x)4

    #h(x) = h1+ _m2

    22gA21 "1

    D1

    D(x)4

    #Note: Untuk perhitungan tekanan teoritis pada titik 2, 3, 4, 5, 6, 7, 8, dan 9,

    jarak diukur dari titik 1 dan tekanan pada titik 1 dianggap tekanan masuk.

    Hitung % error antara nilai teori diatas dengan hasil percobaan.

    %ERROR = jhcalc hexpj

    hexp 100%%ERROR =

    jhcalc hexpj

    hexp 100%

    atau

    A

    BC

    D

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    %ERROR = jhcalc hexpj

    hcalc 100%%ERROR =

    jhcalc hexpj

    hcalc 100%

    Pilihan tergantung pada nilai mana yang saudara anggap lebih teliti (beri alasan

    terhadap nilai yang dianggap teliti tersebut!). Isikan pada Tabel 3.

    (c) Grafikkan xh vs.x untuk nilai teoritis dan percobaan untuk setiap flow ratesecara terpisah.

    (d) UntukVenturi meter dan Orifice meter, plot Cvs.NRe dan bandingkan dengan

    textbook. Beri komentar.

    (e) Plot head loss untuk rotameter vs. kecepatan fluida.

    5. Diskusi

    (a) Jelaskan apakah anggapan Bernoulli terbukti pada percobaan ini?

    (b) Perhatikan pada bagian venturi, uraikan apa yang dimaksud dengan head

    recovery? Mengapa dapat terjadi? Apakah hal serupa terjadi pada orifice?

    Mengapa?

    (c) Beri komentar terhadap plot Cvs.NReVenturi meter dan Orifice meter. Apakah

    nilai flow rate yang akan diukur berpengaruh terhadap ukuran alat yang sebaiknya

    dipakai?

    (d) Coba amati pola alir (dengan mengamati gerakan/lintasan kotoran yang melayang

    bersama aliran). Dapatkah pola alir ini membantu menjelaskan keterangan saudara

    pada bagian (a). Uraikan argumentasi saudara!(e) Manakah alat ukur yang paling hemat energi? Manakah yang paling sensitif?

    Manakah yang paling sederhana?

    (f) Berbagai alat ukur tersebut ada yang korelasi antara bacaan dan flow rate bersifat

    linear. Ada pula yang tidak. Sebutkan masing-masing. Manakah yang lebih baik,

    linear atau non linear, ditinjau dari segi kalibrasi, segi pemakaian?

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    Table 2Nilai tekanan percobaan sebagai fungsi flow rate: m dalam (kg/sec) danh dalam (mm air).

    Q m(kg/sec)

    h1 h2 h3 h4 h5 h6 h7 8h 9h

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    Table 3Nilai teoritis tekanan sebagai fungsi flow-rate: m (kg/sec) danh (mm air).

    Q

    m (kg/sec)

    h1

    % error inh1

    h2

    % error inh2

    h3

    % error inh3

    h4

    % error inh4

    h5

    % error inh5

    h6

    % error inh6

    h7

    % error inh7

    h8

    % error inh8

    h9

    % error inh9