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FLOW OF FLUID
Ms. Deepika Bairagee
Assistant Professor (Quality Assurance)
OCPR, Oriental University, Indore
CONTENT
Definition
Fluid properties
Reynolds experiment
Manometer
Orificemeter
Venturimeter
Pitot tube
Rotameter
 A fluid is a substance that continually deforms (flows) under an
applied shear stress.
 Fluids are a subset of the phases of matter and include liquids,
gases.
 Fluid flow may be defined as the flow of substances that do not
permanently resist distortion
 The subject of fluid flow can be divided into fluid static's and fluid
dynamics
FLUID FLOW
THE PROPERTIES OF FLUIDS
VISCOSITY
SURFACE TENSION
Viscosity is a measure of a fluid's resistance to flow
 It describes the internal friction of a moving fluid.
 A fluid with large viscosity resists motion because
its molecular makeup gives it a lot of internal
friction.
 A fluid with low viscosity flows easily because its
molecular makeup results in very little friction
when it is in motion.
SURFACE TENSION
"Surface tension is a contractive tendency of
the surface of a fluid that allows it to resist an
external force."
Fluid tends to attend the minimum surface as possible
Why?
1. The reason behind this is that while a molecule
inside the fluid bulk is pulled in each and every
direction by the adjacent molecules
2. But at the surface of the fluid , the case is different.
The adhesive forces causes downward pull on the
molecule due to cohesent.
3. So the molecule on the surface tends to move down.
σ = F/L
Unit = N/m
FLUID STATICS
 Fluid static's deals with the fluids at rest in equilibrium
 Behavior of liquid at rest
 Nature of pressure it exerts and the variation of pressure at
different layers
Pressure differences between layers of liquids
h1
h2
Point 1
Point 2
Ps
• Consider a column of liquid with two openings Which are
provided at the wall of the vessel at different height
• The rate of flow through these openings are different due
to the pressure exerted at the different heights are
different
• Consider a stationary column the pressure P is acting on the
surface of the fluid, column is maintained at constant
pressure by applying pressure
• The force acting below and above the point 1 are
evaluated
• Substituting the force with pressure x area of cross section in
the above equation
At point 1
Force acting on the liquid = +
Force on thesurface Force excreted by the liquid
Above point1
P1S = PsS + volume x density x g
Pressure at point 1 x Area= (Pressure on the surface x surface area)+ (mass x g)
Substituting the force with pressure X area of cross section in the above equation
= PsS + height x area x density x g
Since surface area is same
Similarly, the pressure acting on the liquid at point 2
By subtracting equation
FLUID DYNAMICS
Fluid dynamics deals with the study of fluids in motion
• This knowledge is important for liquids, gels, ointments
which will change their flow behavior when exposed to
different stress conditions
Mixing
Flow Through
Pipes
Filled in
Container
Importance
Identification of type of flow is important in Manufacture of
dosage forms & Handling of drugs for administration
• The flow of fluid through a pipe can be viscous or
turbulent and it can be determined by Reynolds
number
• Reynolds number have no unit
Reynolds Experiment
• Glass tube is connected to reservoir of water, rate of flow
of water is adjusted by a valve,
• A reservoir of colored solution is connected to one
end of the glass tube with help of nozzle.
• Colored solution is introduced into the nozzle as
fine stream through jet tube.
water
valve
Colored liquid
LAMINAR OR VISCOUS FLOW
TURBULENT FLOW
Diagram is showing the
flow
TYPES OF FLOW
• Laminar flow is one in which
the fluid particles move in
layers or laminar with one
layer sliding with other
• There is no exchange of
fluid particles from one
layer to other
• Avg velocity = 0.5 Vmax
Re < 2000
• When velocity of the water is
increased the thread of the
colored water disappears and
mass of the water gets
uniformly colored
• There is complete mixing of
the solution and the flow of the
fluid is called as turbulent flow
• Avg velocity = 0.8 Vmax è
Re >4000
The velocity at which the fluid changes from laminar flow to turbulent flow that velocity is called as
critical velocity
REYNOLDS NUMBER
In Reynolds experiment the flow conditions are affected by
Diameter of pipe
Averagevelocity
Density ofliquid
Viscosity of thefluid
This four factors are combined in one way as Reynolds number
Re=
• Inertial forces are due to mass and the velocity of the fluid particles
trying to diffuse the fluid particles
• viscous force if the frictional force due to the viscosity of the fluid which
make the motion of the fluid in parallel.
D u ρ
η
INERTIAL FORCES
= ------------------------------
VISCOUS FORCES
 At low velocities the inertial forces are less when compared
to the frictional forces
 Resulting flow will be viscous innature
 Other hand when inertial forces are predominant the fluid
layers break up due to the increase in velocity hence turbulent
flow takes place.
 If Re < 2000 the flow is said to belaminar
 If Re > 4000 the flow is said to beturbulent
 If Re lies between 2000 to 4000 theflow change between
laminar to turbulent
APPLICATIONS
• Reynolds number is used to predict the nature of the flow
• Stocks law equation is modified to include Reynolds number
to study the rate of sedimentation in suspension
When velocity is plotted against the distance from the wall
following conclusions can be drawn
• The flow of fluid in the middle of the pipe is faster then the
fluid near to the wall
• At the actual surface of the pipe – wall the velocity of the
fluid is zero
BERNOULLI'S THEOREM
When the principles of the law of energy is applied to the flow of the
fluids the resulting equation is a Bernoulli's theorem
• Consider a pump working under isothermal conditions between points A
and B
• Bernoulli's theorem statement, "In a steady state the total energy per
unit mass consists of pressure, kinetic and potential energies are
constant"
Kinetic energy = u2 / 2g
Pump
Pressure energy = Pa / ρAg
Friction energy = F
A
B
Ø At point a one kilogram of liquid is assumed to be entering at point a,
Pressure energy = PA /g ρ A
Where PA = Pressure at point a
g = Acceleration due to gravity ρ A = Density of
theliquid
Potential energy of a body is defined as the energy possessed by the body by the virtue of
its position
Potential energy = XA
Kinetic energy of a body is defined as the energy possessed by the body by virtue of its
motion,
kinetic energy = U2
A/ 2g
Total energy at point A = Pressure energy + Potential energy +K. E Total energy at point
A = PA /g ρ A +XA+U 2
A/ 2g
According to the Bernoulli's theorem the total energy at point A is constant
Total energy at point A = PA / ρ A g +XA+ (UA2/ 2g) = Constant
After the system reaches the steady state, whenever one kilogram of liquid enters at
point A, another one kilogram of liquid leaves at point B
Total energy at point B = PB /ρB g +XB+ (UB2/ 2g) = Constant
INPUT = OUTPUT
Total Energy at point A = Total Energy at Point B
PA / ρ A g +XA+ (UA2/ 2g) = PB /ρ B g +XB+ (UB2/ 2g)
Theoretically all kinds of the energies involved in fluid flow should be accounted,
pump has added certain amount of energy.
During the transport some energy is converted to heat due to frictional
Forces
Energy loss due to friction in the line = F Energy
added by pump = W
PA /ρ A +XA + UA
2 / 2g – F + W = PB /ρ B +XB +UB2/ 2g
This equation is called as Bernoulli's equation
ENERGY LOSS
According to the law of conversation of energy, energy
balance have to be properly calculated fluids experiences
energy losses in several ways
while flowing through pipes, they are
•Frictional losses
•Losses in the fitting
•Enlargement losses
•Contractionlosses
Application of
BERNOULLI'S THEOREM
• Used in the measurement of rateof fluid flow
using flowmeters
• It applied in the working of the centrifugal
pump, in this kinetic energy is converted in to
pressure.
MANOMETERS
Manometers are the devices used for measuring
the pressure difference
Different type of manometers are there they are
1)Simple manometer
2)Differential manometer
3)Inclined manometer
 This manometer is the most commonly used
one
 It consists of a glass U shaped tube filled with a
liquid A- of density ρA kg /meter cube and above A
the arms are filled with liquid B of density ρB
 The liquid A and B are immiscible and the
interference can be seen clearly
 If two different pressures are applied on the two
arms the meniscus of the one liquid will be
higher than the other
SIMPLE MANOMETER
Let pressure at point 1 will be P1 Pascal's and
point 5 will be P2 Pascal's
The pressure at point 2 can be written as
=P1+ (m + R )ρB g
since ∆P = ∆ h ρ g
(m + R ) = distance from 3 to 5
Since the points 2 and 3 are at same height the pressure
Pressure at 3 =P1+ (m + R ) ρ B g
Pressure at 4 is less than pressure at point 3 by R
=P2+ m ρ B g
In another manner, the pressure at point 4
= P1+ (m + R ) ρ Bg - Rρ Ag
This can be summarise as
P1 + (m + R ) ρB g - R ρA g =P2 + gmρB
P1-P2 = gmρB- (m + R ) ρBg + R ρA g
∆P = gmρB – mρBg - RρBg + R ρA g
∆P=R (ρ A- ρ B )g
Application
• Pressure difference can be determined
by measuring R
• Manometers are use in measuring flow of
fluid.
DIFFERENTIAL MANOMETERS
• These manometers are suitable for measurement of small
pressure differences
• It is also known as two – Fluid U- tube manometer
• It contains two immiscible liquids A and B having nearly
same densities
• The U tube contains of enlarged chambers on both limbs,
• Using the principle of simple manometer the pressure
differences can be written as , ∆P =P1 –P2 =R (ρc – ρA)g
Diffrential Manometer
Pressure at different points
Diffrential Manometer
∆P =P1 –P2 =R (ρc – ρA) g
Hence smaller the difference between
ρcand ρAlarger will be R
INCLINED TUBE MANOMETERS
Many applications require accurate measurement of low pressure such
as drafts and very low differentials, primarily in air and gas installations.
In these applications the manometer is arranged with the indicating tube
inclined,
This enables the measurement of small pressure changes with
increased accuracy.
P1 –P2 = g R (ρ A - ρ B) sin α
sin α=R/Ri
R=Risin α
MEASUREMENT OF RATE OF FLOW OF
FLUIDS
Methods of measurement are
Direct weighing ormeasuring
Hydrodynamicmethods
•Orifice meter
•Venturi meter
•Pitot meter
•Rotameter
Direct displacement meter
DIRECT WEIGHING OR
MEASURING
The liquid flowing through a pipe is collected for
specific period at any point and weighed or
measured, and the rate of flow can be determined.
Gases can not be determined by this method
ORIFICE METER
Variable head meter
Principle
o Orifice meter is a thin plate containing a narrow and sharp aperture.
o When a fluid stream is allowed to pass through a narrow constriction
the velocity of the fluid increase compared to up stream
o This results in decrease in pressure head and the difference in the
pressure may be read from a manometer
CONSTRUCTION
• It is consider to be a thin plate containing a sharp aperture through which
fluid flows
• Normally it is placed between long straight pipes
• For present discussion plate is introduced into pipe and manometer is
connected at points A and B
WORKING
• When fluid is allowed to pass through the orifice the velocity of the fluid at
point B increase, as a result at point A pressure will be increased.
• Difference in the pressure is measured by manometer
• Bernoulli's equation is applied to point A and point B for experimental
conditions
Bernaulis eqn...
PA /ρ A +XA + UA / 2g – F + W = PB /ρ B +XB + UB / 2g2 2
UB
2 - UA
2 = 2gc.PA /ρ-2gc.PB/ρ
No work is done on the liquid or by the liquid, w = 0
UB
2 - UA
2 = 2gc/ρ (PA –PB)
√UB
2- UA
2 = √2gc∆H
As (PA - PB)/ρ=∆H
Assumptions
• Pipeline is horizantal A and B are at same position
Therefore XA=XB
• Suppose friction losses are neglisible F=0
• As liquid is incompressible so density remain same,
Therefore ρ A=ρ B=ρ
• No work is done on liquid therefore w=0
Applications
• §Velocity at either of the point A and B can
be measured
• § Volume of liquid flowing perhour can be
determined by knowing area of cross section
VENTURI METER
Variable head meter
Principle
• When fluid is allowed to pass through narrow venturi throat
then velocity of fluid increases and pressure decreases
• Difference in upstream and downstream pressure head
can be measured by using Manometer
• U v = C v √ 2g . ∆H
VENTURI METER
Why Venturi meter if Orifice meter is available?
• Main disadvantage of orifice meter is power loss due to
sudden contraction with consequent eddies on other
side of orifice plate
• We can minimize power loss by gradual
contraction of pipe
• Ventury meter consist of two tapperd (conical section)
inserted in pipeline
• Friction losses and eddies can be minimized by this
arrangement.
DISADVANTAGES
Ø Expensive
Ø Need technical export
Ø Not flexible it is permanent
ADVANTAGES
Ø For permanent installations
Ø Power loss is less
Ø Head loss is negligible
Pitot tube
(Insertion meter)
Principle of Pitot tube
According to Bernoulli's therom
Total energy at any point =
Pressure energy + Potential energy +K. E
U0 = C 0 √ 2g∆H ........∆H= Difference in pressure head
∆H = U2 /2g ........U= Velocity at point of incertion
Pitot tube
CONSTRUCTION
• It is also known as insertion meter
• The size of the sensing element is small compared
to the flow channel
• One tube is perpendicular to the flow direction and
the other is parallel to the flow
• Two tubes are connected to the manometer
2g∆Hp = U2
WORKING
• Pitot tube is used to measure the velocity head of flow.
• Parallel tube (to Upstream) measure velocity head +
pressure head
• Perpendicular tube (downstream) measure only
pressure head
• Difference of head between two tubes gives velocity
head ∆H.
• Working of pitot tube video
Difference between venturi-
orifice and Pitot tube
• Orifice and venturi
meter measure
average velocity of
whole stream of fluid
• More pressure drop
• Pitot tube measure
relative fluid velocity
at single point only
• Less pressure drop
ROTAMETER
Variable area meter
PRINCIPLE
 In this device a stream of water enters Transparent
tapered tube and strikes the moving plummet
 During fluid flow plummet rise orfall
 As a result, annular space(area) between plummet and
tapperd tube may increase or decrease, depending on
variation of flow rate.
 Head across annulus is equal to weight of plummet.
CONSTRUCTION
• It consists of vertically tapered and transparent tube
generally made of glass in which a plummet is centrally
placed with guiding wire.
• Linear scale is etched on glass
• During the flow the plummetrise due to variation in flow
• The upper edge of the plummet is used as an index to note
the reading
WORKING
• As the flow is upward through the tapered tube the
plummet rises and falls depend on the flow rate
• Greater the flow rate higher the rise of plummet.
• Working of rotameter
USE
• To measure flow rate of gas as well as liquid
• Easy to use and allow direct visual inspection
Thank You

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Fluid flow

  • 1. FLOW OF FLUID Ms. Deepika Bairagee Assistant Professor (Quality Assurance) OCPR, Oriental University, Indore
  • 3.  A fluid is a substance that continually deforms (flows) under an applied shear stress.  Fluids are a subset of the phases of matter and include liquids, gases.  Fluid flow may be defined as the flow of substances that do not permanently resist distortion  The subject of fluid flow can be divided into fluid static's and fluid dynamics FLUID FLOW
  • 4. THE PROPERTIES OF FLUIDS VISCOSITY SURFACE TENSION
  • 5. Viscosity is a measure of a fluid's resistance to flow  It describes the internal friction of a moving fluid.  A fluid with large viscosity resists motion because its molecular makeup gives it a lot of internal friction.  A fluid with low viscosity flows easily because its molecular makeup results in very little friction when it is in motion.
  • 6. SURFACE TENSION "Surface tension is a contractive tendency of the surface of a fluid that allows it to resist an external force."
  • 7. Fluid tends to attend the minimum surface as possible Why? 1. The reason behind this is that while a molecule inside the fluid bulk is pulled in each and every direction by the adjacent molecules 2. But at the surface of the fluid , the case is different. The adhesive forces causes downward pull on the molecule due to cohesent. 3. So the molecule on the surface tends to move down.
  • 9. FLUID STATICS  Fluid static's deals with the fluids at rest in equilibrium  Behavior of liquid at rest  Nature of pressure it exerts and the variation of pressure at different layers Pressure differences between layers of liquids h1 h2 Point 1 Point 2 Ps
  • 10. • Consider a column of liquid with two openings Which are provided at the wall of the vessel at different height • The rate of flow through these openings are different due to the pressure exerted at the different heights are different • Consider a stationary column the pressure P is acting on the surface of the fluid, column is maintained at constant pressure by applying pressure • The force acting below and above the point 1 are evaluated • Substituting the force with pressure x area of cross section in the above equation
  • 11. At point 1 Force acting on the liquid = + Force on thesurface Force excreted by the liquid Above point1 P1S = PsS + volume x density x g Pressure at point 1 x Area= (Pressure on the surface x surface area)+ (mass x g) Substituting the force with pressure X area of cross section in the above equation = PsS + height x area x density x g Since surface area is same Similarly, the pressure acting on the liquid at point 2 By subtracting equation
  • 12. FLUID DYNAMICS Fluid dynamics deals with the study of fluids in motion • This knowledge is important for liquids, gels, ointments which will change their flow behavior when exposed to different stress conditions Mixing Flow Through Pipes Filled in Container
  • 13. Importance Identification of type of flow is important in Manufacture of dosage forms & Handling of drugs for administration • The flow of fluid through a pipe can be viscous or turbulent and it can be determined by Reynolds number • Reynolds number have no unit
  • 14. Reynolds Experiment • Glass tube is connected to reservoir of water, rate of flow of water is adjusted by a valve, • A reservoir of colored solution is connected to one end of the glass tube with help of nozzle. • Colored solution is introduced into the nozzle as fine stream through jet tube.
  • 15. water valve Colored liquid LAMINAR OR VISCOUS FLOW TURBULENT FLOW
  • 16.
  • 17. Diagram is showing the flow
  • 18. TYPES OF FLOW • Laminar flow is one in which the fluid particles move in layers or laminar with one layer sliding with other • There is no exchange of fluid particles from one layer to other • Avg velocity = 0.5 Vmax Re < 2000 • When velocity of the water is increased the thread of the colored water disappears and mass of the water gets uniformly colored • There is complete mixing of the solution and the flow of the fluid is called as turbulent flow • Avg velocity = 0.8 Vmax è Re >4000 The velocity at which the fluid changes from laminar flow to turbulent flow that velocity is called as critical velocity
  • 19. REYNOLDS NUMBER In Reynolds experiment the flow conditions are affected by Diameter of pipe Averagevelocity Density ofliquid Viscosity of thefluid This four factors are combined in one way as Reynolds number Re= • Inertial forces are due to mass and the velocity of the fluid particles trying to diffuse the fluid particles • viscous force if the frictional force due to the viscosity of the fluid which make the motion of the fluid in parallel. D u ρ η INERTIAL FORCES = ------------------------------ VISCOUS FORCES
  • 20.  At low velocities the inertial forces are less when compared to the frictional forces  Resulting flow will be viscous innature  Other hand when inertial forces are predominant the fluid layers break up due to the increase in velocity hence turbulent flow takes place.  If Re < 2000 the flow is said to belaminar  If Re > 4000 the flow is said to beturbulent  If Re lies between 2000 to 4000 theflow change between laminar to turbulent
  • 21. APPLICATIONS • Reynolds number is used to predict the nature of the flow • Stocks law equation is modified to include Reynolds number to study the rate of sedimentation in suspension When velocity is plotted against the distance from the wall following conclusions can be drawn • The flow of fluid in the middle of the pipe is faster then the fluid near to the wall • At the actual surface of the pipe – wall the velocity of the fluid is zero
  • 22. BERNOULLI'S THEOREM When the principles of the law of energy is applied to the flow of the fluids the resulting equation is a Bernoulli's theorem • Consider a pump working under isothermal conditions between points A and B • Bernoulli's theorem statement, "In a steady state the total energy per unit mass consists of pressure, kinetic and potential energies are constant" Kinetic energy = u2 / 2g Pump Pressure energy = Pa / ρAg Friction energy = F A B
  • 23. Ø At point a one kilogram of liquid is assumed to be entering at point a, Pressure energy = PA /g ρ A Where PA = Pressure at point a g = Acceleration due to gravity ρ A = Density of theliquid Potential energy of a body is defined as the energy possessed by the body by the virtue of its position Potential energy = XA Kinetic energy of a body is defined as the energy possessed by the body by virtue of its motion, kinetic energy = U2 A/ 2g Total energy at point A = Pressure energy + Potential energy +K. E Total energy at point A = PA /g ρ A +XA+U 2 A/ 2g
  • 24. According to the Bernoulli's theorem the total energy at point A is constant Total energy at point A = PA / ρ A g +XA+ (UA2/ 2g) = Constant After the system reaches the steady state, whenever one kilogram of liquid enters at point A, another one kilogram of liquid leaves at point B Total energy at point B = PB /ρB g +XB+ (UB2/ 2g) = Constant INPUT = OUTPUT Total Energy at point A = Total Energy at Point B PA / ρ A g +XA+ (UA2/ 2g) = PB /ρ B g +XB+ (UB2/ 2g) Theoretically all kinds of the energies involved in fluid flow should be accounted, pump has added certain amount of energy.
  • 25. During the transport some energy is converted to heat due to frictional Forces Energy loss due to friction in the line = F Energy added by pump = W PA /ρ A +XA + UA 2 / 2g – F + W = PB /ρ B +XB +UB2/ 2g This equation is called as Bernoulli's equation
  • 26. ENERGY LOSS According to the law of conversation of energy, energy balance have to be properly calculated fluids experiences energy losses in several ways while flowing through pipes, they are •Frictional losses •Losses in the fitting •Enlargement losses •Contractionlosses
  • 27. Application of BERNOULLI'S THEOREM • Used in the measurement of rateof fluid flow using flowmeters • It applied in the working of the centrifugal pump, in this kinetic energy is converted in to pressure.
  • 28. MANOMETERS Manometers are the devices used for measuring the pressure difference Different type of manometers are there they are 1)Simple manometer 2)Differential manometer 3)Inclined manometer
  • 29.  This manometer is the most commonly used one  It consists of a glass U shaped tube filled with a liquid A- of density ρA kg /meter cube and above A the arms are filled with liquid B of density ρB  The liquid A and B are immiscible and the interference can be seen clearly  If two different pressures are applied on the two arms the meniscus of the one liquid will be higher than the other SIMPLE MANOMETER
  • 30. Let pressure at point 1 will be P1 Pascal's and point 5 will be P2 Pascal's The pressure at point 2 can be written as =P1+ (m + R )ρB g since ∆P = ∆ h ρ g (m + R ) = distance from 3 to 5
  • 31. Since the points 2 and 3 are at same height the pressure Pressure at 3 =P1+ (m + R ) ρ B g Pressure at 4 is less than pressure at point 3 by R =P2+ m ρ B g In another manner, the pressure at point 4 = P1+ (m + R ) ρ Bg - Rρ Ag This can be summarise as P1 + (m + R ) ρB g - R ρA g =P2 + gmρB P1-P2 = gmρB- (m + R ) ρBg + R ρA g ∆P = gmρB – mρBg - RρBg + R ρA g ∆P=R (ρ A- ρ B )g
  • 32. Application • Pressure difference can be determined by measuring R • Manometers are use in measuring flow of fluid.
  • 33. DIFFERENTIAL MANOMETERS • These manometers are suitable for measurement of small pressure differences • It is also known as two – Fluid U- tube manometer • It contains two immiscible liquids A and B having nearly same densities • The U tube contains of enlarged chambers on both limbs, • Using the principle of simple manometer the pressure differences can be written as , ∆P =P1 –P2 =R (ρc – ρA)g
  • 36. Diffrential Manometer ∆P =P1 –P2 =R (ρc – ρA) g Hence smaller the difference between ρcand ρAlarger will be R
  • 37. INCLINED TUBE MANOMETERS Many applications require accurate measurement of low pressure such as drafts and very low differentials, primarily in air and gas installations. In these applications the manometer is arranged with the indicating tube inclined, This enables the measurement of small pressure changes with increased accuracy. P1 –P2 = g R (ρ A - ρ B) sin α
  • 39. MEASUREMENT OF RATE OF FLOW OF FLUIDS Methods of measurement are Direct weighing ormeasuring Hydrodynamicmethods •Orifice meter •Venturi meter •Pitot meter •Rotameter Direct displacement meter
  • 40. DIRECT WEIGHING OR MEASURING The liquid flowing through a pipe is collected for specific period at any point and weighed or measured, and the rate of flow can be determined. Gases can not be determined by this method
  • 41. ORIFICE METER Variable head meter Principle o Orifice meter is a thin plate containing a narrow and sharp aperture. o When a fluid stream is allowed to pass through a narrow constriction the velocity of the fluid increase compared to up stream o This results in decrease in pressure head and the difference in the pressure may be read from a manometer
  • 42.
  • 43. CONSTRUCTION • It is consider to be a thin plate containing a sharp aperture through which fluid flows • Normally it is placed between long straight pipes • For present discussion plate is introduced into pipe and manometer is connected at points A and B WORKING • When fluid is allowed to pass through the orifice the velocity of the fluid at point B increase, as a result at point A pressure will be increased. • Difference in the pressure is measured by manometer • Bernoulli's equation is applied to point A and point B for experimental conditions
  • 44. Bernaulis eqn... PA /ρ A +XA + UA / 2g – F + W = PB /ρ B +XB + UB / 2g2 2 UB 2 - UA 2 = 2gc.PA /ρ-2gc.PB/ρ No work is done on the liquid or by the liquid, w = 0 UB 2 - UA 2 = 2gc/ρ (PA –PB) √UB 2- UA 2 = √2gc∆H As (PA - PB)/ρ=∆H
  • 45. Assumptions • Pipeline is horizantal A and B are at same position Therefore XA=XB • Suppose friction losses are neglisible F=0 • As liquid is incompressible so density remain same, Therefore ρ A=ρ B=ρ • No work is done on liquid therefore w=0
  • 46. Applications • §Velocity at either of the point A and B can be measured • § Volume of liquid flowing perhour can be determined by knowing area of cross section
  • 47. VENTURI METER Variable head meter Principle • When fluid is allowed to pass through narrow venturi throat then velocity of fluid increases and pressure decreases • Difference in upstream and downstream pressure head can be measured by using Manometer • U v = C v √ 2g . ∆H
  • 49. Why Venturi meter if Orifice meter is available? • Main disadvantage of orifice meter is power loss due to sudden contraction with consequent eddies on other side of orifice plate • We can minimize power loss by gradual contraction of pipe • Ventury meter consist of two tapperd (conical section) inserted in pipeline • Friction losses and eddies can be minimized by this arrangement.
  • 50.
  • 51. DISADVANTAGES Ø Expensive Ø Need technical export Ø Not flexible it is permanent ADVANTAGES Ø For permanent installations Ø Power loss is less Ø Head loss is negligible
  • 52.
  • 53. Pitot tube (Insertion meter) Principle of Pitot tube According to Bernoulli's therom Total energy at any point = Pressure energy + Potential energy +K. E U0 = C 0 √ 2g∆H ........∆H= Difference in pressure head ∆H = U2 /2g ........U= Velocity at point of incertion
  • 55.
  • 56. CONSTRUCTION • It is also known as insertion meter • The size of the sensing element is small compared to the flow channel • One tube is perpendicular to the flow direction and the other is parallel to the flow • Two tubes are connected to the manometer 2g∆Hp = U2
  • 57. WORKING • Pitot tube is used to measure the velocity head of flow. • Parallel tube (to Upstream) measure velocity head + pressure head • Perpendicular tube (downstream) measure only pressure head • Difference of head between two tubes gives velocity head ∆H. • Working of pitot tube video
  • 58. Difference between venturi- orifice and Pitot tube • Orifice and venturi meter measure average velocity of whole stream of fluid • More pressure drop • Pitot tube measure relative fluid velocity at single point only • Less pressure drop
  • 60. PRINCIPLE  In this device a stream of water enters Transparent tapered tube and strikes the moving plummet  During fluid flow plummet rise orfall  As a result, annular space(area) between plummet and tapperd tube may increase or decrease, depending on variation of flow rate.  Head across annulus is equal to weight of plummet.
  • 61. CONSTRUCTION • It consists of vertically tapered and transparent tube generally made of glass in which a plummet is centrally placed with guiding wire. • Linear scale is etched on glass • During the flow the plummetrise due to variation in flow • The upper edge of the plummet is used as an index to note the reading
  • 62. WORKING • As the flow is upward through the tapered tube the plummet rises and falls depend on the flow rate • Greater the flow rate higher the rise of plummet. • Working of rotameter USE • To measure flow rate of gas as well as liquid • Easy to use and allow direct visual inspection