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Title: Practical%20Aspects%20of%20using%20Pitot%20Tube


1
Practical Aspects of using Pitot Tube
  • P M V Subbarao
  • Professor
  • Mechanical Engineering Department

Corrections to Devotion from Potential Flow
2
YAW AND PITCH ANGLE RANGE
  • If the fluid stream is not parallel to the probe
    head, errors occur in both total and static
    readings. 
  • These are the most important errors in this type
    of instrument because they cannot be corrected
    without taking independent readings with another
    type of probe.

3
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4
Errors due to Yaw and Pitch Angle
5
WALL BOUNDARY EFFECTS
  • The static pressure indication is sensitive to
    distance from solid boundaries. 
  • The probe and boundary form a Venturi passage,
    which accelerates the flow and decreases the
    static pressure on one side. 

6
y/d
The curve shows that static readings should not
be taken closer than 5 tube diameters from a
boundary for 1 accuracy and 10 tube diameters is
safer.
7
TURBULENCE ERRORS
  • Pitot-Static tubes appear to be insensitive to
    isotropic turbulence, which is the most common
    type. 
  • Under some conditions of high intensity, large
    scale turbulence, could make the angle of attack
    at a probe vary over a wide range.
  • This probe would presumably have an error
    corresponding to the average yaw or pitch angle
    produced by the turbulence

8
TIME CONSTANT
  • The speed of reading depends on
  • the length and diameter of the pressure passages
    inside the probe,
  • the size of the pressure tubes to the manometer,
    and
  • the displacement volume of the manometer. 
  • The time constant is very short for any of the
    standard tubes down to 1/8" diameter.
  • It increases rapidly for smaller diameters. 
  • For this reason 1/16" OD is the smallest
    recommended size for ordinary use .
  • This will take 15 to 60 seconds to reach
    equilibrium pressure with ordinary manometer
    hook-ups. 

9
  • The tubes have been made as small as 1/32" OD.
  • But their time constant is as long as 15 minutes
    and they clog up very easily with fine dirt in
    the flow stream. 
  • If very small tubes are required, it is
    preferable to use separate total and static tubes
    rather than the combined total-static type. 
  • Where reinforcing stems are specified on small
    sizes, the inner tubes are enlarged at the same
    point to ensure minimum time constant.

10
Dynamic response of a Pitot-Static Tube
11
Assumptions
  • The fluid is assumed to be incompressible the
    total length of the fluid column remains fixed at
    L.
  • Assume that the probe is initially in the
    equilibrium position.
  • The pressure difference ?p is suddenly applied
    across it.
  • The fluid column will move during time t gt 0.

12
The forces that are acting on the length L of the
fluid are
Force disturbing the equilibrium
Inertial Force
Forces opposing the change a. Weight of column
of fluid
b. Fluid friction due to viscosity of the fluid
  • The velocity of the fluid column is expected to
    be small and the laminar assumption is thus
    valid.
  • The viscous force opposing the motion is
    calculated based on the assumption of fully
    developed Hagen-Poiseuelle flow.

The fricitional pressure drop
13
Newtons Law of Motion
14
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15
Second Order System
The essential parameters
The static sensitivity
The dimensionless damping ratio
The Natural Frequency
16
Transfer Function of a second order system for
step input
17
  • The transfer function is parameterized in terms
    of ? and ?n.
  • The value of ?n doesnt qualitatively change the
    system response.
  • There are three important caseswith
    qualitatively different system behavioras ?
    varies.
  • The three cases are called
  • Over Damped System (? gt1)
  • Critically Damped System (? 1)
  • Under Damped System (? lt1)

18
General Response of A Second Order System
t
z0
y(t)
t
z0.5
19
z0.707
z1.0
t
20
Response of Pitot tube to step input
21
  • Over Damped System (? gt1)

22
y(t)
t
23
Measurement of Multi-dimensional Flows
24
Five Hole Probes
  • The five-hole probe is an instrument often used
    in low-speed wind tunnels to measure flow
    direction, static pressure, and total pressure in
    subsonic flows.
  • This adaptation permits extending the useful
    calibration range up to 85 .
  • A special calibration is to been done, and new,
    extended range calibration curves are to be
    provided.

25
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26
Probe Description
  • The probe consists of four direction-sensing
    ports plus a center port, precision bored into a
    conical brass tip.
  • Four individual small diameter stainless steel
    tubes connect the four side sensing ports to
    individual pressure transducers.
  • The outer 3.175 millimeter diameter tube serves
    as the pressure transmitting channel for the
    center tube, as well as housing for the four
    side-port tubes.
  • This small 3.175 millimeter tube is fitted within
    a larger tube for increased stiffness away from
    the sensing tip.

27
Calibration of Five Hole Probes
28
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29
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