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FLUID MECHANICS – 1
      Semester 1 2011 - 2012



           Week – 9



   FLOW MEASUREMENT
          CO4


  Compiled and modified
           by
     Sharma, Adam
Chapters to cover


     1. Properties of Fluid
     2. Fluid Statics
     3. Fluid in Motion
     4. Friction in Piping System
     5. Flow Measurement




                                    2
Chapters to cover


     1. Properties of Fluid
     2. Fluid Statics
     3. Fluid in Motion
     4. Friction in Piping System
     5. Flow Measurement




                                    3
Flow Measurement

•   Explain type of flow measuring
    equipments
•   Calculate fluid flow through
    –   Pitot tube,
    –   Orifice meter,
    –   Venturi meter
    –   Nozzle meter.
                                     4
Types of Flowmeters
                                        F lo w m e t e r s

P re ssu re              M e c h a n ic a l            T h e rm a l                  O th e r
  Types                     Types                        Types                       Types

       O r ific e s               T u r b in e                H o t-w ir e                   V o rte x
     flo w m e te r             flo w m e te r               flo w m e te r               flo w m e te r

   V e n tu ri T u b e        R e c ip o c a te in g    R e s is tiv e -b r id g e   E le c tr o m a g n e tic
     flo w m e te r         P is to n flo w m e te r         flo w m e te r               flo w m e te r

     F lo w T u b e             O v a l-G e a r                 O th e rs                U ltr a s o n ic
     flo w m e te r             flo w m e te r                                           F lo w m e te r

   F lo w N o z z le s             O th e rs                                                O th e rs
      flo w m e te r

    P ilo t T u b e s
     flo w m e te r

       O th e r s

                                                                                                                 5
Pitot Tube



                   1
                          P2 2
                P1,V1     Stagnation
                          Point V2=0


 P1 is a Static pressure: It is measured by a device (static tube)
 that causes no velocity change to the flow. This is usually
 accomplished by drilling a small hole normal to a wall along
 which the fluid is flowing.

 P2 is a Stagnation pressure: It is the pressure measured by an
                                                                      6
 open-ended tube facing the flow direction. Such a device is
Pitot Tube
The basic pitot tube simply consists of a tube pointing directly into the
fluid flow. The fluid is at rest or stagnant inside the tube. A pressure is
created in the stagnant tube that is greater than the pressure of the
fluid stream. The magnitude of this increased pressure is related to
the velocity of the moving fluid. The pressure of the moving fluid is
called the static pressure.




    (a) A Pitot probe measures stagnation pressure at the nose of
    the probe, while (b) a Pitot-static probe measures both
    stagnation pressure and static pressure, from which the flow              7
    speed is calculated.
Pitot-Static Tube
The static and Pitot tube are often combined into the one-piece Pitot-static
tube.

                                      Examples
                                      Used in
                                      aircraft
                                      nose




                                                                               8
Pitot-Static Tube
Stagnation
pressure tap
                    Static pressure tap




               2      V1 = 0
  V     1             z1 = z2




                                          9
Obstruction Flowmeters:
Orifice, Venturi, and
Nozzle Meters
Flowmeters based on this principle
are called obstruction flowmeters
and are widely used to measure flow
rates of gases and liquids.

                                      Flow through a constriction in a pipe.




                                                                        10
The losses can be accounted for by incorporating a correction factor called the
discharge coefficient Cd whose value (which is less than 1) is determined
experimentally.




The value of Cd depends on both b and the Reynolds number, and
charts and curve-fit correlations for Cd are available for various types of
obstruction meters.




For flows with high Reynolds numbers (Re > 30,000), the value of
                                                                                  11
Cd can be taken to be 0.96 for flow nozzles and 0.61 for orifices.
Common types of obstruction meters.

                                      12
Pipe Flowrate Meters
     Example 1: Flow through an orifice meter
  The flow rate of water at 20°C (ρ = 998 kg/m3 and μ = 1.002x10-3 kg/m ·
  s) through a 50-cm-diameter pipe is measured with an orifice meter
  with a 30-cm-diameter opening to be 250 L/s. Determine the pressure
  difference
  indicated by the orifice meter and the head loss. The discharge
  coefficient of the orifice meter is Cd = 0.61.




                                                                            13
Pipe Flowrate Meters
 Assumptions 1 The flow is steady and incompressible. 2 The discharge
 coefficient of the orifice meter is Cd = 0.61.

 Properties The density and dynamic viscosity of water are given
 to be ρ = 998 kg/m3 and μ = 1.002x10-4 kg/ms, respectively.

 Analysis The diameter ratio and the throat area of the orifice are

  β = d D = 30 50 = 0.60
  A0 = πd 2 4 = π (0.3) 2 4 = 0.07069 m 2
 For a pressure drop of                across the orifice plate, the flow
 rate is expressed as ∆P   = P − P2
                              1



                  2( P − P2 )
 Q = AoCd             1
                    (
                  ρ 1− β 4    )
                                                                            14
Pipe Flowrate Meters
 Substituting,
                                                     2∆P
                 (
0.25m /s = 0.07069 m
        3                    2
                                 )( 0.61) (                )(
                                              998 kg/m 3 1 − 0.60 4        )
This gives a pressure drop
of,
 ∆p = 14600 kg.m/s = 14.6 kPa
                      2



 We know,
 ∆P = ρgh
                                                   This is the head loss
 then,
     ∆P   14600
 h=     =           = 1.49 m
     ρg (998)(9.81)
Pipe Flowrate Meters
 Venturi Meter
 This device consists of a conical contraction, a short cylindrical
 throat and a conical expansion. The fluid is accelerated by being
 passed through the converging cone. The velocity at the “throat”
 is assumed to be constant and an average velocity is used. The
 venturi tube is a reliable flow measuring device that causes little
 pressure drop. It is used widely particularly for large liquid and gas
 flows.




             P1             P2




                                                                    16
Pipe Flowrate Meters
 Venturi Meter




                       17
Pipe Flowrate Meters
 Venturi Meter




                                 2( p1 − p2 )
  Qactual = CVQideal = C V A T
                                 ρ (1 − β 4 )
  AT = π d 2 / 4    Area of the throat
  CV = CV (β = d / D, Re = ρ VD / µ )



                                                18
Pipe Flowrate Meters
Venturi Meter

   A Venturi meter equipped with a differential pressure gage is
   used to measure the flow rate of water at 15°C (ρ = 999.1 kg/m3)
   through a 5-cm-diameter horizontal pipe. The diameter of the
   Venturi neck is 3 cm, and the measured pressure drop is 5 kPa.
   Taking the discharge coefficient to be 0.98, determine the
   volume flow rate of water and the average velocity through the
   pipe.




                                                                      19
Pipe Flowrate Meters
 Assumptions 1 The flow is steady and incompressible. 2 The discharge
 coefficient of the venturi meter is Cd = 0.98.

 Properties The density and dynamic viscosity of water are given
 to be ρ = 999.1 kg/m3 and.

 Analysis The diameter ratio and the throat area of the orifice are

β = d D = 3 5 = 0.60
A0 = πd 2 4 = π (0.03) 2 4 = 0.0007069 m 2
 For a pressure drop of                across the orifice plate, the flow
 rate is expressed as ∆P   = 5 kPa

                  2( P − P2 )
 Q = AoCd             1
                    (
                  ρ 1− β 4    )
                                                                            20
Pipe Flowrate Meters
 Substituting,

           (
Q m /s = 7.069 ×10 m
    3                  -4    2
                                 )( 0.98) (          2(5000)
                                                          )(
                                              999.1 kg/m 3 1 − 0.60 4   )
This gives a flow rate of,

Q = 0.00235 m /s = 2.35 liters/s
                  3



 Average velocity in pipe is,
   Q   Q     0.00235 m 3 /s
 V= =      =                = 1.20 m/s
   A ρD / 4 π (0.05 m ) / 4
       2             2




                                                                   21
Pipe Flowrate Meters
 Nozzle Meter




                                 2( p1 − p2 )
Qactual = C n Qideal = C n A n
                                 ρ(1 − β4 )
 A n = πd 2 / 4 Area of the hole
 C n = C n (β = d / D, Re = ρVD / µ )
 Nozzle meter discharge coefficient

                                                22
Pipe Flowrate Meters
Nozzle Meter
  A flow nozzle equipped with a differential pressure gage is used to
  measure the flow rate of water at 10°C (ρ= 999.7 kg/m3 and μ = 1.307
  x 10-3 kg/m · s) through a 3-cm-diameter horizontal pipe. The nozzle
  exit diameter is 1.5 cm, and the measured pressure drop is 3 kPa.
  The nozzle has a discharge coefficient of Cd= 0.96.Determine the
  volume flow rate of water, the average velocity through the pipe,
  and the head loss.




                                                                         23
It’s the same!!!!!!!!!!!
All equations

                                  2( p1 − p2 )            ORIFICE
 Qactual = CoQideal = Co A o
                                  ρ (1 − β 4 )

                               2( p1 − p2 )               VENTURI
Qactual = C VQideal = CV A T
                               ρ (1 − β 4 )

                                    2( p1 − p 2 )
 Qactual = C n Qideal = C n A n                           NOZZLE
                                    ρ(1 − β4 )



                                                                    24
25
26
27
Pitot-Static Tube
 An object is traveling at an elevation of 10,000
 m in standard atmosphere. The pressure
 difference indicated by the Pitot-static probe
 attached to the roof is 2000 Pa. What is the
 velocity of the object? (The density of air at
 this altitude is 0.414 kg/m3)
                      Pitot-static




                                                28
29

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9. fm 9 flow measurement co 4 adam

  • 1. FLUID MECHANICS – 1 Semester 1 2011 - 2012 Week – 9 FLOW MEASUREMENT CO4 Compiled and modified by Sharma, Adam
  • 2. Chapters to cover 1. Properties of Fluid 2. Fluid Statics 3. Fluid in Motion 4. Friction in Piping System 5. Flow Measurement 2
  • 3. Chapters to cover 1. Properties of Fluid 2. Fluid Statics 3. Fluid in Motion 4. Friction in Piping System 5. Flow Measurement 3
  • 4. Flow Measurement • Explain type of flow measuring equipments • Calculate fluid flow through – Pitot tube, – Orifice meter, – Venturi meter – Nozzle meter. 4
  • 5. Types of Flowmeters F lo w m e t e r s P re ssu re M e c h a n ic a l T h e rm a l O th e r Types Types Types Types O r ific e s T u r b in e H o t-w ir e V o rte x flo w m e te r flo w m e te r flo w m e te r flo w m e te r V e n tu ri T u b e R e c ip o c a te in g R e s is tiv e -b r id g e E le c tr o m a g n e tic flo w m e te r P is to n flo w m e te r flo w m e te r flo w m e te r F lo w T u b e O v a l-G e a r O th e rs U ltr a s o n ic flo w m e te r flo w m e te r F lo w m e te r F lo w N o z z le s O th e rs O th e rs flo w m e te r P ilo t T u b e s flo w m e te r O th e r s 5
  • 6. Pitot Tube 1 P2 2 P1,V1 Stagnation Point V2=0 P1 is a Static pressure: It is measured by a device (static tube) that causes no velocity change to the flow. This is usually accomplished by drilling a small hole normal to a wall along which the fluid is flowing. P2 is a Stagnation pressure: It is the pressure measured by an 6 open-ended tube facing the flow direction. Such a device is
  • 7. Pitot Tube The basic pitot tube simply consists of a tube pointing directly into the fluid flow. The fluid is at rest or stagnant inside the tube. A pressure is created in the stagnant tube that is greater than the pressure of the fluid stream. The magnitude of this increased pressure is related to the velocity of the moving fluid. The pressure of the moving fluid is called the static pressure. (a) A Pitot probe measures stagnation pressure at the nose of the probe, while (b) a Pitot-static probe measures both stagnation pressure and static pressure, from which the flow 7 speed is calculated.
  • 8. Pitot-Static Tube The static and Pitot tube are often combined into the one-piece Pitot-static tube. Examples Used in aircraft nose 8
  • 9. Pitot-Static Tube Stagnation pressure tap Static pressure tap 2 V1 = 0 V 1 z1 = z2 9
  • 10. Obstruction Flowmeters: Orifice, Venturi, and Nozzle Meters Flowmeters based on this principle are called obstruction flowmeters and are widely used to measure flow rates of gases and liquids. Flow through a constriction in a pipe. 10
  • 11. The losses can be accounted for by incorporating a correction factor called the discharge coefficient Cd whose value (which is less than 1) is determined experimentally. The value of Cd depends on both b and the Reynolds number, and charts and curve-fit correlations for Cd are available for various types of obstruction meters. For flows with high Reynolds numbers (Re > 30,000), the value of 11 Cd can be taken to be 0.96 for flow nozzles and 0.61 for orifices.
  • 12. Common types of obstruction meters. 12
  • 13. Pipe Flowrate Meters Example 1: Flow through an orifice meter The flow rate of water at 20°C (ρ = 998 kg/m3 and μ = 1.002x10-3 kg/m · s) through a 50-cm-diameter pipe is measured with an orifice meter with a 30-cm-diameter opening to be 250 L/s. Determine the pressure difference indicated by the orifice meter and the head loss. The discharge coefficient of the orifice meter is Cd = 0.61. 13
  • 14. Pipe Flowrate Meters Assumptions 1 The flow is steady and incompressible. 2 The discharge coefficient of the orifice meter is Cd = 0.61. Properties The density and dynamic viscosity of water are given to be ρ = 998 kg/m3 and μ = 1.002x10-4 kg/ms, respectively. Analysis The diameter ratio and the throat area of the orifice are β = d D = 30 50 = 0.60 A0 = πd 2 4 = π (0.3) 2 4 = 0.07069 m 2 For a pressure drop of across the orifice plate, the flow rate is expressed as ∆P = P − P2 1 2( P − P2 ) Q = AoCd 1 ( ρ 1− β 4 ) 14
  • 15. Pipe Flowrate Meters Substituting, 2∆P ( 0.25m /s = 0.07069 m 3 2 )( 0.61) ( )( 998 kg/m 3 1 − 0.60 4 ) This gives a pressure drop of, ∆p = 14600 kg.m/s = 14.6 kPa 2 We know, ∆P = ρgh This is the head loss then, ∆P 14600 h= = = 1.49 m ρg (998)(9.81)
  • 16. Pipe Flowrate Meters Venturi Meter This device consists of a conical contraction, a short cylindrical throat and a conical expansion. The fluid is accelerated by being passed through the converging cone. The velocity at the “throat” is assumed to be constant and an average velocity is used. The venturi tube is a reliable flow measuring device that causes little pressure drop. It is used widely particularly for large liquid and gas flows. P1 P2 16
  • 17. Pipe Flowrate Meters Venturi Meter 17
  • 18. Pipe Flowrate Meters Venturi Meter 2( p1 − p2 ) Qactual = CVQideal = C V A T ρ (1 − β 4 ) AT = π d 2 / 4 Area of the throat CV = CV (β = d / D, Re = ρ VD / µ ) 18
  • 19. Pipe Flowrate Meters Venturi Meter A Venturi meter equipped with a differential pressure gage is used to measure the flow rate of water at 15°C (ρ = 999.1 kg/m3) through a 5-cm-diameter horizontal pipe. The diameter of the Venturi neck is 3 cm, and the measured pressure drop is 5 kPa. Taking the discharge coefficient to be 0.98, determine the volume flow rate of water and the average velocity through the pipe. 19
  • 20. Pipe Flowrate Meters Assumptions 1 The flow is steady and incompressible. 2 The discharge coefficient of the venturi meter is Cd = 0.98. Properties The density and dynamic viscosity of water are given to be ρ = 999.1 kg/m3 and. Analysis The diameter ratio and the throat area of the orifice are β = d D = 3 5 = 0.60 A0 = πd 2 4 = π (0.03) 2 4 = 0.0007069 m 2 For a pressure drop of across the orifice plate, the flow rate is expressed as ∆P = 5 kPa 2( P − P2 ) Q = AoCd 1 ( ρ 1− β 4 ) 20
  • 21. Pipe Flowrate Meters Substituting, ( Q m /s = 7.069 ×10 m 3 -4 2 )( 0.98) ( 2(5000) )( 999.1 kg/m 3 1 − 0.60 4 ) This gives a flow rate of, Q = 0.00235 m /s = 2.35 liters/s 3 Average velocity in pipe is, Q Q 0.00235 m 3 /s V= = = = 1.20 m/s A ρD / 4 π (0.05 m ) / 4 2 2 21
  • 22. Pipe Flowrate Meters Nozzle Meter 2( p1 − p2 ) Qactual = C n Qideal = C n A n ρ(1 − β4 ) A n = πd 2 / 4 Area of the hole C n = C n (β = d / D, Re = ρVD / µ ) Nozzle meter discharge coefficient 22
  • 23. Pipe Flowrate Meters Nozzle Meter A flow nozzle equipped with a differential pressure gage is used to measure the flow rate of water at 10°C (ρ= 999.7 kg/m3 and μ = 1.307 x 10-3 kg/m · s) through a 3-cm-diameter horizontal pipe. The nozzle exit diameter is 1.5 cm, and the measured pressure drop is 3 kPa. The nozzle has a discharge coefficient of Cd= 0.96.Determine the volume flow rate of water, the average velocity through the pipe, and the head loss. 23
  • 24. It’s the same!!!!!!!!!!! All equations 2( p1 − p2 ) ORIFICE Qactual = CoQideal = Co A o ρ (1 − β 4 ) 2( p1 − p2 ) VENTURI Qactual = C VQideal = CV A T ρ (1 − β 4 ) 2( p1 − p 2 ) Qactual = C n Qideal = C n A n NOZZLE ρ(1 − β4 ) 24
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  • 28. Pitot-Static Tube An object is traveling at an elevation of 10,000 m in standard atmosphere. The pressure difference indicated by the Pitot-static probe attached to the roof is 2000 Pa. What is the velocity of the object? (The density of air at this altitude is 0.414 kg/m3) Pitot-static 28
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