DR UFOEGBUNAM M.P
DEPARTMENT OF ANAESTHESIA UNTH ENUGU
INTRODUCTION
 Both gases and liquids are termed fluids
 Liquids are incompressible and at constant
temperature occupy a fixed volume and conforming to
the shape of a container
 Gases have no fixed volume but expand to occupy the
total space of a container
FLOW
 Defined as the quantity of fluids(Gas,liquid or vapour) that
passes a point per unit time. A simple equation to represent
this is
 Flow(F) = Quantity (Q)
 Time(t)
 Flow is sometimes written as ∆Q (rate of change of a
quantity, mass or volume)
 Due to the quantities of different fluids that are given to
our patients during a routine anaesthesia, flow is an
important area of physics to understand
Consider for following questions
 Why are the scales on ratometers (flow meters) non-
uniform as flow increases?, why are there different
rotameters for different gases
 Under what circumstances is Heliox useful and why?
 Will there be much difference ventilating through a size
4 endotracheal tube compared to a size 8 endotracheal
tube?
 How much more fliud can be administered through a
14G cannula than a 22G cannula?
Flow of fluids
 Viscosity is defined as that property of a fluid which
causes it to resist flow. The coefficient of viscosity (п)
is defined as
 (п) = force × velocity gradient/Area
 In this context, velocity gradient is equal to the
difference between velocities of different fluid
molecules divided by the distance between molecules
Cont..
 The units of the coefficient of viscosity are Pascal
seconds
 Fliuds which obey this formula are reffered to as
newtonian fluids and cofficient of viscosity is a
constant for each fluid
 Some biological fluids are non- newtonian e.g Blood
 Viscosity of liquids diminishes with increasing temp.
where as viscosity of gas increases with increasing
temperature
Types of flow
 Flow can be divided into two different types
 Laminar flow
 Turbulent flow
 A number of different physical characteristics
determine whether a fluid obeys the principle of one
or the other
Laminar flow through tubes
 A tube is a cylideriacal vessel whose length is much more
than the diameter
 Hagen-Poiseuille’s (1799-1868) law: the flow rate is
proportional to the perfussion pressure, also proportional to
the fourth power of the radius and inversely proportional to
the length and coefficient of viscosity
 Q = π(P1 –P2)r4
 ή8L
 Laminar flow is smooth, streamlined and noiseless
Turbulent flow through tubes
 It occurs when flow exceeds a critical value
 Turbulence is facilitated by irregularities and corners
in the tube.
 Conversion from laminar to turbulent flow increases
resistance, which itself becomes roughly proportional
to flow
 The dimensionless Reynolds number (Re) must exceed
2000 for turbulence to occur
CONT..
 Re = diameter×density×average velocity/Viscosity
 Turbulent flow is noisy, less ordered and eddy currents
interfere with each other, increasing drag or resistance to
flow.
 Turbulent flow occurs when fluids flow at high velocity in
large diameter tubes and when the fluids are relatively
dense
 Decreasing the velocity of a fliud leads to turbulent flow
Cont..
 Measurments in tubes have shown that
 When the Reynolds number is less than 2000, there is
laminar flow
 When the Reynolds number is 2000-4000 there is
transitional flow ie. A mixture of laminar and turbulent
flow
 When the Reynolds number is greater than 4000 flow
will be turbulent
Flow through orifices
 An orifice is an opening whose length is much less than
its diameter. It causes turbulence and the resistance to
flow is related to the gas density rather than viscosity
 Helium- oxygen mixture (Heliox) may be useful in upper
airway obstruction because the mixture is less dense
than Oxygen or Air
 In Rotameters or flowmeters, the gas flow around the
bobbin is laminar at low- flow rates, so viscosity is
important. At high flows, the annular aperture around
the bobbin resembles an orifice and density is important
Venturi principle
 Described in 1797 (Giovanni venturi, an Italian
physicist)
 When fluid flows through a tube of varying diameter,
the pressure is lowest at the point of maximum
velocity, because pressure energy drops as kinetic
energy increases
 Also similarly described by Bernoulli(1700-1782
 With suitable flow and a “venturi” cone shaped tube,
subatmospheric pressure can easily be produced
Cont..
 The injector replaces the smooth contruction of a
venturi tube with a nozzle through which fliud is
injected at high velocity. Surrounding fliuds are
sucked in with the main stream
 Suction apparatus
 Entrainment of air or oxygen during therapy
 Jet ventilation eg. By Sanders injector during bronchoscopy
THANK YOU

DYNAMICS OF FLOW.ppt

  • 1.
    DR UFOEGBUNAM M.P DEPARTMENTOF ANAESTHESIA UNTH ENUGU
  • 2.
    INTRODUCTION  Both gasesand liquids are termed fluids  Liquids are incompressible and at constant temperature occupy a fixed volume and conforming to the shape of a container  Gases have no fixed volume but expand to occupy the total space of a container
  • 3.
    FLOW  Defined asthe quantity of fluids(Gas,liquid or vapour) that passes a point per unit time. A simple equation to represent this is  Flow(F) = Quantity (Q)  Time(t)  Flow is sometimes written as ∆Q (rate of change of a quantity, mass or volume)  Due to the quantities of different fluids that are given to our patients during a routine anaesthesia, flow is an important area of physics to understand
  • 4.
    Consider for followingquestions  Why are the scales on ratometers (flow meters) non- uniform as flow increases?, why are there different rotameters for different gases  Under what circumstances is Heliox useful and why?  Will there be much difference ventilating through a size 4 endotracheal tube compared to a size 8 endotracheal tube?  How much more fliud can be administered through a 14G cannula than a 22G cannula?
  • 5.
    Flow of fluids Viscosity is defined as that property of a fluid which causes it to resist flow. The coefficient of viscosity (п) is defined as  (п) = force × velocity gradient/Area  In this context, velocity gradient is equal to the difference between velocities of different fluid molecules divided by the distance between molecules
  • 6.
    Cont..  The unitsof the coefficient of viscosity are Pascal seconds  Fliuds which obey this formula are reffered to as newtonian fluids and cofficient of viscosity is a constant for each fluid  Some biological fluids are non- newtonian e.g Blood  Viscosity of liquids diminishes with increasing temp. where as viscosity of gas increases with increasing temperature
  • 7.
    Types of flow Flow can be divided into two different types  Laminar flow  Turbulent flow  A number of different physical characteristics determine whether a fluid obeys the principle of one or the other
  • 8.
    Laminar flow throughtubes  A tube is a cylideriacal vessel whose length is much more than the diameter  Hagen-Poiseuille’s (1799-1868) law: the flow rate is proportional to the perfussion pressure, also proportional to the fourth power of the radius and inversely proportional to the length and coefficient of viscosity  Q = π(P1 –P2)r4  ή8L  Laminar flow is smooth, streamlined and noiseless
  • 9.
    Turbulent flow throughtubes  It occurs when flow exceeds a critical value  Turbulence is facilitated by irregularities and corners in the tube.  Conversion from laminar to turbulent flow increases resistance, which itself becomes roughly proportional to flow  The dimensionless Reynolds number (Re) must exceed 2000 for turbulence to occur
  • 10.
    CONT..  Re =diameter×density×average velocity/Viscosity  Turbulent flow is noisy, less ordered and eddy currents interfere with each other, increasing drag or resistance to flow.  Turbulent flow occurs when fluids flow at high velocity in large diameter tubes and when the fluids are relatively dense  Decreasing the velocity of a fliud leads to turbulent flow
  • 11.
    Cont..  Measurments intubes have shown that  When the Reynolds number is less than 2000, there is laminar flow  When the Reynolds number is 2000-4000 there is transitional flow ie. A mixture of laminar and turbulent flow  When the Reynolds number is greater than 4000 flow will be turbulent
  • 12.
    Flow through orifices An orifice is an opening whose length is much less than its diameter. It causes turbulence and the resistance to flow is related to the gas density rather than viscosity  Helium- oxygen mixture (Heliox) may be useful in upper airway obstruction because the mixture is less dense than Oxygen or Air  In Rotameters or flowmeters, the gas flow around the bobbin is laminar at low- flow rates, so viscosity is important. At high flows, the annular aperture around the bobbin resembles an orifice and density is important
  • 13.
    Venturi principle  Describedin 1797 (Giovanni venturi, an Italian physicist)  When fluid flows through a tube of varying diameter, the pressure is lowest at the point of maximum velocity, because pressure energy drops as kinetic energy increases  Also similarly described by Bernoulli(1700-1782  With suitable flow and a “venturi” cone shaped tube, subatmospheric pressure can easily be produced
  • 14.
    Cont..  The injectorreplaces the smooth contruction of a venturi tube with a nozzle through which fliud is injected at high velocity. Surrounding fliuds are sucked in with the main stream  Suction apparatus  Entrainment of air or oxygen during therapy  Jet ventilation eg. By Sanders injector during bronchoscopy
  • 15.