Advanced Air Duct Design Part 1

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    Method of Duct Design Lecture No.(1) By Badran M. Salem

    1

    Advanced Air Duct Design

    Introduction

    Correct air diffusion, as well as the proper quantity of conditional air

    conditioned, is essential for comfortable conditions in forced systems. A

    well designed air duct system, either commercial or industrial, must

    consider most of the following system design factors: (1) space

    availability; (2) space air diffusion; (3) noise levels; (4) duct leakage; (5)

    duct heat gain and losses; (6) balancing; (7) fire and smoke control; (8)

    initial investment cost; (9) system operating cost.

    Any deficiency in duct design may result in a system that does not

    operate properly. These deficiencies include system, which are

    excessively expensive to own and / or operate. Poor air distribution can

    cause discomfort, and lack sound attenuators may result in objectionable

    noise levels. Poor duct construction or lack of duct sealing can cause

    inadequate airflow rates at the terminal units. Inadequate airflow is also

    caused by excessive heat gains/losses, which can be avoided with proper

    duct insulation. Poor design of the branches concerning main ducts may

    result in unbalanced systems. As a part of our course, we redesigned the

    duct system in the building. Moreover, we resized all the ducts depending

    on the actual data that we have calculated.

    Duct Design MethodsThe most common methods of air duct system design are: (1) equal

    friction, velocity reduction, static regain and variations such as total

    pressure, and constant velocity. The choice of design method is the

    designer s and the system design with the minimum owning and

    operating cost depends on both the application and ingenuity of the

    designer. No single duct design method will automatically produce the

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    Method of Duct Design Lecture No.(1) By Badran M. Salem

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    progressively in the direction of the return intakes. With the ducts sized

    and the fittings known, the total pressure losses can be calculated, the

    pressure gradients plotted, and the minimum pressure loss or critical path

    of the system established.

    A refinement of this method involves sizing the branch ducts to

    dissipate the pressure available at the entrance to each. The pressure loss

    of the ductwork between the fan and first branch take-off is subtracted

    from the total fan pressure to obtain the available pressure at the first

    junction. Through trial, a branch velocity is found that results in the

    branch pressure loss being equal to or less than the pressure available.The procedure is repeated for each branch.

    Static Regain Method

    The static regain method is design procedure in which the ducts are

    sized so that the increase in static pressure (static regain) at each take-off

    offsets the pressure loss of the succeeding section of ductwork. Thismethod is especially suited for high velocity installations having long

    runs with many take-offs or terminal units. With this design procedure,

    approximately the same static pressure exists at the entrance to each

    branch, which simplifies outlet or terminal unit selection and system

    balancing. With the ductwork sized by this method, the systems total

    pressure losses can be calculated. The major disadvantage of this method,however, is that excessively large ducts (low velocities) result at the end

    of long duct runs.

    The total pressure design method is adaptation of the static regain

    method. This method is advantageous since a designer has knowledge of

    the intermediate system pressures and control of duct sizes and velocities.

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    Method of Duct Design Lecture No.(1) By Badran M. Salem

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    Constant Velocity Method

    Since the constant velocity design method is generally applied to

    exhaust systems conveying particulates, and since these systems are

    usually round, this method is applied for round ducts only.

    Duct Design Procedures

    The general procedure for duct design is as follows:

    1. Study the plans of the building and arrange the supply and return

    outlets to provide proper distribution of air within each space. Adjustcalculated actual air quantities for duct heat gains or losses and duct

    leakage. Also, adjust the supply, return, and/or exhaust air quantities

    to meet space pressurization requirements.

    2. Select outlet sizes from manufacturers data.

    3. Sketch the duct system, connecting the supply outlets and return

    intakes with the central station apparatus, taking recognizance of the building construction, and avoiding all structural obstructions and

    equipment. The space allocated for the supply and return ducts often

    dictates the system layout and the shape of the ductwork.

    4. Determine the size of main and all branches by the selected design

    method.

    5.

    Calculate the total pressure requirements of all duct sections, bothsupply and return, and then plot the total pressure grade line.

    6. To design a system with the minimum owning and operating costs,

    repeat steps 4 and 5 with different duct sizes. It is necessary to

    estimate the cost of the initial design and the incremental cost

    variations due to the redesigns.

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    Method of Duct Design Lecture No.(1) By Badran M. Salem

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    7. Layout the system in detail. If significant duct routing and fitting

    variations have occurred from the original design, recalculate the

    pressure losses.

    8. Redesign the duct branches to minimize the balancing necessary by

    dampers.

    9. Analyze the design for objectionable noise levels and specify sound

    attenuators as necessary.

    10. Select the fan.

    Air Duct Design

    Equal Friction Method

    This method is used to determine the diameter of air duct, so that

    the duct friction loss per unit length at various duct section always remain

    constant. The final dimensions of sized ducts should be rounded to

    standard size. The procedure of this method is as follows:

    1. Select a suitable velocity in the main duct from sound level

    considerations as given in the table.

    2. Knowing the air flow rate from the load estimation.

    3. The sized of the main duct and friction loss are determined.

    4. The remaining ducts are then sized respectively.

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    Method of Duct Design Lecture No.(1) By Badran M. Salem

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    Example:

    The system shown below, find the size of the main duct and branches.

    First we will use the Equal friction method.

    The main duct A-B.

    The total flow rate is,

    smQ

    QQQQ

    t

    t

    /8134 3221

    We assume the velocity in the main duct A B and size the duct

    md

    V d Q

    smV

    t

    128.1884

    4

    /82

    Friction losses in the main duct A-B

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    Method of Duct Design Lecture No.(1) By Badran M. Salem

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    2

    2V d fL

    P

    Assume the roughness of the surface from the table and calculate the

    value,

    000133.0128.1

    00015.0d

    We can calculate the Reynolds number for air in the main duct after

    finding the viscosity and density of the air from the table.

    The properties of the air is at 25 oC.

    56 1080.510413.18

    128.18184.1Re

    Vd

    From Moody chart, we can find the fraction factor, f

    m Pa L P

    Pa P

    f

    /487.0

    61.142

    8128.1

    300145.0184.1

    0145.02

    The branch B-E.

    42

    22

    2

    82

    ,4

    d

    QV

    d

    QV

    AV Q

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    Method of Duct Design Lecture No.(1) By Badran M. Salem

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    smd Q

    V

    m L P

    fQ

    d

    d Q

    d f

    L P

    /281.54

    491.0487.0

    10145.0184.188

    8

    2

    525 2

    2

    42

    2

    By using the value of d and V, we can calculate the Reynolds number

    again and modify the value of d and V if possible as follows,

    The first modification of d and V gives,

    000305.0491.0

    00015.0

    1066.110413.18

    491.0281.5184.1Re 56

    d

    Vd

    016.0 f

    smV

    md

    /073.5

    501.0

    The second modification of d and V gives,

    016.0

    000299.0513.0

    00015.0

    1063.110413.18501.0073.5184.1

    Re 56

    f d

    Vd

    The same fraction factor, so the value of d and V does not change.

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    Method of Duct Design Lecture No.(1) By Badran M. Salem

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    smV

    md

    /073.5

    501.0

    We can check the volume flow rate is less or higher the design value,

    smV d AV Qcal /000069.1073.5501.044322

    This is acceptable value.

    The branch B-C.

    smd Q

    V

    m

    L P

    fQd

    /489.7091.1744

    091.1487.0

    7016.0184.188

    22

    52

    2

    5 2

    2

    The first modification of d and V gives,

    000137.0091.1

    00015.0

    1025.510413.18

    0696.179.7184.1Re 56

    d

    Vd

    0146.0 f

    The same fraction factor we used, so the value of d and V does not

    change.

    smV

    md

    /768.7

    071.1

    The second modification of d and V gives,

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    Method of Duct Design Lecture No.(1) By Badran M. Salem

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    0146.0

    00014.0071.1

    00015.0

    1035.510413.18

    071.1768.7184.1Re 56

    f d

    Vd

    The same fraction factor we used, so the value of d and V does not

    change.

    smV

    md

    /768.7

    071.1

    We can check the volume flow rate is less or higher the design value,

    smV d AV Qcal /998.6768.7071.144322

    This is acceptable value.

    The branch C-F.

    smd Q

    V

    m

    L P

    fQd

    /557.67621.0

    344

    7632.0487.0

    30146.0184.188

    22

    52

    2

    5 2

    2

    The first modification of d and V gives,

    0163.0

    000197.07632.0

    00015.0

    1022.310413.18

    7632.0557.6184.1Re 56

    f

    d

    Vd

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    Method of Duct Design Lecture No.(1) By Badran M. Salem

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    smV

    md

    /275.6

    780.0

    The second modification of d and V gives,

    0164.0

    000192.0780.0

    00015.0

    1015.310413.18

    780.0275.6184.1Re 56

    f d

    Vd

    The same fraction factor we used, so the value of d and V does not

    change.

    smV

    md

    /275.6

    780.0

    We can check the volume flow rate is less or higher the design value,

    smV d AV Qcal /9984.2275.678.044322

    This is acceptable value.

    The branch C-D.

    smd Q

    V

    m

    L P

    fQd

    /630.68551.0

    444

    8764.0487.0

    40164.0184.188

    22

    52

    2

    5 2

    2

    The first modification of d and V gives,

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    Method of Duct Design Lecture No.(1) By Badran M. Salem

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    0157.0

    000171.08764.0

    00015.0

    1074.310413.18

    8764.0630.6184.1Re 56

    f d

    Vd

    smV

    md

    /747.6

    869.0

    The second modification of d and V gives,

    0159.0

    000173.0869.0

    00015.0

    1077.310413.18

    869.0747.6184.1Re 56

    f d

    Vd

    smV

    md

    /747.6

    869.0

    The difference between second and first modification is not so much, so

    the value of d and V does not change.

    We can check the volume flow rate is less or higher the design value,

    smV d AV Qcal /002.4747.6869.044322

    This is acceptable value.

    The results of calculation must be illustrated in a table to use it in the

    calculation of air fan power.

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    Method of Duct Design Lecture No.(1) By Badran M. Salem

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    Results

    Section L (m) Q (m3/s) V (m/s d (m) Qcal

    A-B 30 8 8.00 1.128 8.000

    B-C 15 7 7.77 1.071 6.998

    C-D 75 4 6.75 0.869 4.002

    B-E 30 1 5.07 0.501 1.000

    C-F 15 3 6.275 0.780 2.998

    For galvanized steel air duct and air properties at 20 oC, the following

    charts could be used for estimate the duct size and velocity at a given

    pressure drop per meter and volume flow rate.

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    Method of Duct Design Lecture No.(1) By Badran M. Salem

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    Duct friction chart-low flow rate.

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    Method of Duct Design Lecture No.(1) By Badran M. Salem

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    Duct friction chart-high flow rate.

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    The above two charts recommended only for air and the duct which

    made from galvanized steel with = 0.00015 m and rounded section. But

    if another duct material it should be use correction factor.

    We now recalculate the given example by using the duct chart.

    The main duct A-B.

    The total flow rate is,

    smQ

    QQQQ

    t

    t

    /8134 3221

    We assume the velocity in the main duct A B and size the duct

    smV /8

    From chart at Q = 8 m3/s and V = 8 m/s, the equivalent diameter and pressure loss are,

    m Pa P

    md

    /5.0

    135.1

    We use the value of P=0.5 Pa/m is constant through all branches and

    determine the velocity and diameter from chart and tabulated the resultsas follows,

    Resluts

    Section L (m) Q (m3/s) V (m/s d (m) Qcal

    A-B 30 8 8.00 1.135 8.094

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    Method of Duct Design Lecture No.(1) By Badran M. Salem

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    Velocity Reduction Method

    In this method the main duct is designed in the same manner as in

    the equal friction method. Thereafter, arbitrary reductions are made in the

    air velocity as we go down the duct run. Equivalent diameters are found,

    as before from the friction chart. We now recalculate the given example

    by using the velocity reduction method and using the chart.The main duct A-B.

    The total flow rate is,

    smQ

    QQQQ

    t

    t

    /8134 3221

    We assume the velocity in the main duct A B and size the duct

    smV /8

    From chart at Q = 8 m3/s and V = 8 m/s, the equivalent diameter and

    pressure loss are,

    m Pa P

    md

    /5.0

    135.1

    B-C 15 7 7.8 1.080 7.145

    C-D 75 4 6.9 0.875 4.149

    B-E 30 1 4.80 0.515 0.999

    C-F 15 3 6.30 0.780 3.010

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    We assume the velocity as follows,

    B-C, V = 7 m/s

    B-E, V = 7 m/s, C-D, C-F, V = 6 m/s.

    After that, we determine the duct diameter and friction loss from the chart

    and put the results in table as follows,

    Results

    Section L (m) Q (m3/s) V (m/s d (m) Qcal

    A-B 30 8 8.00 1.135 8.094

    B-C 15 7 7.00 1.130 7.020

    C-D 75 4 6.00 0.925 4.032

    B-E 30 1 7.00 0.430 1.017

    C-F 15 3 6.00 0.800 3.016

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    Method of Duct Design Lecture No.(1) By Badran M. Salem

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    Air Fan Power

    Total, Static and dynamic Pressure.

    Bernoullis equation

    V V

    S T S T V

    T

    V S

    T V S

    T Z V S

    P V

    V P

    P P P P P

    P

    P P

    P P P dZ

    P P P P

    C gZ V

    P

    C gZ V P

    2or

    2

    Pitotube. bymeasuringare,where,

    Pressure.Total:

    PressureDynamicorPressureVelocity:Pressure,Static:Where,

    ,,0If

    2

    2

    2

    2

    2

    For frictionless flow between two sections as follows,

    T V S V S P P P P P 2211

    But due to friction loss

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    Method of Duct Design Lecture No.(1) By Badran M. Salem

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    2.and1 betweenlosseshydraulicordrop pressuretotal:where,2211

    L

    LV S V S

    P

    P P P P P

    If the Fan or Blower is introduced between two section .

    duct.in thedrop pressurelossestherepresents:where,222

    pressure.headFan total the

    calledisandFan workthetoduerise pressuretheiswhere,

    222211

    2211

    L

    LS S

    LV S V S

    h

    hV P W V P

    FTP

    P P P FTP P P

    As flow continues in a duct, the static pressure of air continuously drops.

    This drop in pressure takes place due to two factors,

    Duct to friction (friction loss)

    diameter meanhydraulic: where,,2

    2

    d V

    d fL

    P F

    Change of direction or velocity (dynamic loss)

    constant:where,,2

    2

    K V

    K P M

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    Method of Duct Design Lecture No.(1) By Badran M. Salem

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    For Enlargement.

    21122211

    V V S S

    V S V S

    P P P P

    P P P P

    Due to friction loss,

    221121 V S V S T T L P P P P P P P

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    Method of Duct Design Lecture No.(1) By Badran M. Salem

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    Air flow through a simple duct system.

    Suction-side

    Friction of inlet grill, P i :

    )(

    )()(

    Similarly,)(

    )(

    )(

    0

    552215

    52215225

    2212

    2112

    11

    111

    1

    V iS

    iT T

    V iS

    T T

    V iS

    V S iT

    iT

    P P P P P

    P P P P P P

    P P P P

    P P P

    P P P

    P P C P

    P P

    Discharge-side.

    The pressure loss at outlet in discharge grill, P e :

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    Method of Duct Design Lecture No.(1) By Badran M. Salem

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    8865221

    5221886

    56

    6886666

    8868686

    888

    88

    )(

    FTPPressure,TotalFan

    V ei

    iV e

    T T

    V V eV T S

    V eT T

    eV T S

    V eT

    P P P P P P

    P P P P P P

    P P FTP

    P P P P P P P

    P P P P P P

    P P P P

    P P P

    By applying the modified Bernoullis equation between 5 -6,

    Constant, , Z, ,0

    adiabatic,is processfantheIf

    )(2

    656565

    56

    25

    2656

    .

    6565

    Z V V Q

    Z Z g V V P P

    mW Q S S

    886655221.

    552216886

    .

    65

    Power

    Power

    V eV V i

    V iV V e

    P P P P P P P P m

    P P P P P P P P m

    W

    If P V5 =P V6 , V 5 =V 6

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    Method of Duct Design Lecture No.(1) By Badran M. Salem

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    T act

    e

    ed F

    V V K V d L f m

    V P P

    m

    Power Power

    is, powerFanactualThe

    ,efficiencytotalhasFanairtheIf

    222

    2Power

    T

    222.

    2.

    Air Fan System Characteristics.

    Consider a straight air duct system in which the total pressure drop

    is calculated by adding the losses of different sections, which are in turn

    proportional to their respective velocity pressure as follows:

    222

    2.

    2.2.2.

    222

    1211

    211

    21

    21

    21

    21

    21

    21

    21

    A A K

    Ad L

    f V P

    AV

    AV

    K AV

    d L

    f P

    V V K V d L f P

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    Method of Duct Design Lecture No.(1) By Badran M. Salem

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    222

    .2

    2.

    .

    1211

    211

    21

    where,

    ,

    follows,aswirtten becanlossdynamicandfrictionThe

    rate.flowair volumetheistheduct,airof sectiononeFor

    A A K

    Ad L

    f R

    V

    P R

    V R P

    V

    Where, R is the air duct flow resistance. So, by analogy with electricity,

    we can derive the concept of resistance R of the duct system.

    Air Duct System in Series.

    The friction loss and dynamic loss be calculated in each section

    and we use the equation power directly as follow:

    321 P P P P

    Air Duct System in Parallel.

    The friction loss and dynamic loss be calculated in each branch and we

    use the equation power directly as follow:

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    Method of Duct Design Lecture No.(1) By Badran M. Salem

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    321

    321

    .

    3

    .

    2

    .

    1

    .

    1111

    R R R R

    R P

    R P

    R P

    R P

    V V V V

    t

    t

    After could calculate the friction and dynamic loss in air duct system in

    series or in parallel and calculate the equivalent resistance, we will tray to

    calculate the power required in the last example.

    Power of Air FanTo calculate the Fan power we reshape the duct system again

    according to the diameter which we calculated as follows.

    The pressure drop in air handling unit is as follows:

    Damper : 050 Pa

    Filter : 100 Pa

    Cooling coil : 150 Pa

    Eliminators : 050 Pa

    Heating Coil : 150 pa

    Mixing and suction to fan : 050 Pa

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    The dynamic loss coefficients K is as follows:

    Fan discharge to main duct : 0.30Standard 90 oC elbow : 0.75Reduction : 0.05Exit grille : 0.50

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    Reshaping the duct system with air handling unit.

    The Air Duct System can be simplified as follows:

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    Air Handling unit, R 1 :

    4

    22.1

    2

    /12581.78

    527.464

    /527.464

    184.1501505015010050

    mV

    P R

    sm

    P P

    AH

    AH

    Section A-B, R 2 :

    42

    222

    /14285.0)128.130

    0209.03.0(9986.01

    21

    1

    2

    11

    2

    1

    m R Ad

    L f

    A

    K R

    Section B-C, R 3 :

    43

    223

    /12112.0)07.1

    150208.005.0(

    8086.01

    21

    1211

    21

    m R

    Ad L

    f A

    K R

    Section C-D, R 4 :

    44

    4

    224

    /10596.6

    )1868.075

    0225.050.075.005.0(3502.01

    21

    1211

    21

    m R

    R

    Ad L

    f A

    K R

    Section B-E, R 5 :

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    Method of Duct Design Lecture No.(1) By Badran M. Salem

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    45

    5

    225

    /1151.44

    )1513.0

    30026.050.075.0(

    0427.0

    1

    2

    1

    1211

    21

    m R

    R

    Ad L

    f A

    K R

    Section C-F, R 6 :

    46

    6

    226

    /1970.5

    )1778.015

    0232.050.075.0(2259.01

    21

    1211

    21

    m R

    R

    Ad L

    f A

    K R

    R 4 , R 6 in parallel shape, R t1 :

    41

    641

    /15149.1

    970.5

    1

    0596.6

    1111

    m R

    R R R

    t

    t

    R 3 , R t1 in series shape, R t2 : 4

    132 /17261.15149.12112.0 m R R R t t

    R 5 , R t2 in parallel shape, R t3 :

    4

    3

    253

    /120324.1

    7261.1

    1

    151.44

    1111

    m R

    R R R

    t

    t t

    R 1 , R 2 , R t3 in series shape, R t :

    4321 /18895.820324.14282.02581.7 m R R R R t t

    222.

    /930.56888895.8 smV R P P

    t d F

    Fan Power.

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    Method of Duct Design Lecture No.(1) By Badran M. Salem

    31

    KW W V R

    V RV P P

    m

    t

    t d F

    4.5Power 886.538888895.8184.1Power

    Power

    33.

    2...

    A First Approximate Method.

    We can apply the modified Bernoullis equation on the longest line only,from A to D as follows,

    222Power 222.

    eV V d L

    f V

    K mW

    KW

    W DC

    C B

    B AC A

    7.5Power

    948.5679332.97411.10387.27527.4648184.1Power

    2

    78.6)15.075.005.0(

    184.1

    702.075

    279.7

    05.0184.1

    702.015

    28

    3.0184.1

    702.030184.1

    501505015010050

    8184.1Power

    2

    2

    2

    /

    A Second Approximate Method.

    We apply modify Bernoullis equation in all section of the duct system asfollows,

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    Method of Duct Design Lecture No.(1) By Badran M. Salem

    32

    E B

    DC

    C B

    B AC A

    284.4

    )15.075.0(184.1

    702.0301184.1

    278.6

    15.075.005.02

    702.0754184.1

    2

    79.705.0

    184.1

    702.0157184.1

    28

    3.0184.1

    702.030184.1

    5015050150100508184.1Power

    2

    2

    2

    2

    /

    KW

    W F C

    4.5Power

    750.5350806.177263.52037.375234.8641.4659Power

    231.6

    )15.075.0(2702.015

    3184.1

    2

    Problems in Air Duct Design

    1- For air conditioning system shown below, calculate the duct size and

    air velocity in each branch by using equal friction and velocity

    reduction method. For the longest branch A-E and by using modified

    Bernoull equation, estimate the power required for the electric air fan.

    Assume that = 0.13.

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    Method of Duct Design Lecture No.(1) By Badran M. Salem

    33

    Modified Bernoull Equation.

    2- Calculate the duct size and velocity of each branch in the below

    network and also suggest a suitable design structure to calculate the

    power required. The air distributor gives equal flow rate of 15 m 3/min.

    3- In the duct layout shown below, the outlets are deliver 25 m 3/min at 1,

    15 m 3/min at 2 and 30 m 3/min at 3. Also, select air velocity of 8 m/s in

    the section A. Determine the size of duct system using equal friction

    method and determine the static pressure requirement for the air fan.

    22)(222

    12

    21

    2212 V

    K

    V

    d

    fL

    z z g

    V V P P

    mW Qt

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    Method of Duct Design Lecture No.(1) By Badran M. Salem

    34

    4- Size the duct in the problem 3 by using Velocity reduction method and

    find the power required for the air fan.

    5- For a system shown below, size the ducts on a rate of friction pressure

    drop of 0.7536 Pa/m and the air flow rate from the fan is 4 m 3/s. The

    two outlets delivers equal masses of air.

    a) Modify the diameter of branch duct to outlet 1 so that no

    damper is required at the outlet.

    b) Calculate the fan total and static pressure, also the power

    required.

    The pressure drops in each equipment are as follows:

    Filter 100 Pa. Damper 50 Pa.

    Cooling coil 150 Pa. Mixing section 50 Pa.

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    Method of Duct Design Lecture No.(1) By Badran M. Salem

    The dynamic loss coefficient K for all expander are to be taken as

    applying to the difference the upstream and downstream velocity

    pressure, and for all reducers as applying to the downstream velocity

    pressure only. The values are given in the following table.

    SectionK

    Condition

    Inlet 1.4 Mean face velocity = 4 m/s

    Expander AB 0.35M ean face veloci ty at fi l ter = 1.5 m/s

    Reducer BC 0.02 Mean face velocity at damper = 3 m/s

    Reducer EF to fan section 0.02

    Reducer GH at fan

    discharge

    0.3

    Straight through duct

    suction.

    0.25

    Elbow 0.23

    Grille 0.5