ExperimentsClass3Handouts

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AOE 3054

Measuring Velocity and Pressure in

Fluid Flows

• Relevant to experiments 3 and 7, senior lab

• See Barlow et al., “Low Speed Wind

Tunnel Testing” for more info

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AOE 3054 - Class 10

Measuring Velocity and Pressure in

Fluid Flows

• Why?
• What characteristics should measurement devices

have?

• Pressure measurement techniques

Transducers

(Manometer, diaphragm, piezo-electric)

Probes

(Tap, standard, other devices)

• Velocity measurement techniques

Pitot-static probe
Hot-wire anemometry
Laser Doppler anemometry

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Why Measure Pressure or Velocity?



• to understand the flow (to enable prediction)
• to evaluate the performance of a device
• to evaluate the likely effects of the flow
• to obtain other information (e.g. lift, drag)

What Characteristics Should

Measurement Devices Have?

= flow
problem
diagnosis and
resolution

e.g. velocity measurement
in a turbulent flow of
40m/s with scales as
small as 1mm = dynamic
response of 40kHz needed

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Flows can be dynamic…

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Pressure measurement - Transducers

h

A. Manometer


p

1

p

2

Inclined manometer

Multi-tube manometer

p

atm

p

1

p

2

p

3

...

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Pressure measurement - Transducers

B. Piezo-electric, Piezo-resistive


v

out

Charge

Amplifier or

Bridge Circuit

and Amp

Crystal

p

2

p

1

C. Diaphragm Type

• Measures -

p

2

- p

1

d

Transducer is described as Differential, if p

2

comes from flow

Absolute, if p

2

= 0 (vacuum), Gage, if p

2

= p

atm,

Reference, if p

2

= some reference pressure

• Accuracy/limitations/response - Depends on technique
used to sense diaphragm deflection (see next slide)

d

p

1

p

2

Piezo-electric transducers

Piezo-resistive

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C. Diaphragm Type

Methods for sensing diaphragm deflection

1. LVDT ?

• Accuracy/limitations –

• Dynamic response –

Iron core slides
in and out of
transformer
changing coupling between coils and
therefore output AC voltage

2. Strain gage

• Accuracy/limitations -

• Dynamic response -

Strain gages wired as

arms of Wheatstone-bridge

circuit sense deflection

Ametec

AM747X

LVDT

transducer

Ranges from

30 to 6000psig

Honeywell A-5

4-arm strain gage

transducer. Ranges

from 0.5 to

30000psia

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C. Diaphragm Type

Methods for sensing diaphragm deflection

3. Capacitance (microphone)

• Accuracy/limitations -

• Dynamic response -

C

2

C

1

Insulator

Difference in

capacitance between

diaphragm and two

sides varies with

deflection

http://www.setra.com/

Setra Model 239

Ranges 0.15" H

2

O to 10psid

No dynamic response

Bruel and Kjaer Model 4938

0.25" diameter mike

Dynamic response from 4Hz to 70kHz

3"

0.25"

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Pressure measurement - Probes

A. Pressure Tap / Flush mount


tube to transducer

(poor response)

Microphone:

small cavity =

good response

Flush‘Kulite’ piezo:

good response

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Example

Instrumented Blade

NACA 0012, 2’ chord, 6’ span

96 Sennheiser KE 4-211-2 microphones

Signal conditioning for each microphone
(operating circuitry, signal amplifiers)
inside blade to minimize interference.
64-channel, 16-bit data acquisition at
56kHz

Chordwise resolution - 1%c near leading
edge

Spanwise spacing - 1%c to 96%c

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Pressure measurement - Probes

B. The Static Probe

• Measures -

• Accuracy -

• Dynamic response -

C. Other Devices

to transducer

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Velocity measurement

The Pitot-Static Probe

• Measures -

• Accuracy/Limitations -





• Dynamic response -

p

p

0

U

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Velocity measurement

The Pitot-Static Probe

Pitot static misalignment errors

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Example

F-15B/Flight Test Fixture: an

aerodynamics and fluid

dynamics research test bed at

NASA Dryden Flight

Research Center (Edwards,

California).

Rake of Pitot probes for measuring

velocity at different heights in a/c

boundary layer

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Velocity measurement

The Yaw Probe

U

V

W

• Typically one central hole and 4 or 6
surrounding on a conical or
hemispherical probe tip.
• Each hole connected to a separate
transducer.
• Requires extensive calibration
varying independently all 3 velocity
components
• Diameter variable, typically 3mm

See

http://www.aeroprobe.com/products.html

for real examples

• Measures -
• Accuracy/Limitations -





• Dynamic response -

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Velocity measurement

Hot-Wire Anemometry - Probes

• Measures -

Accuracy/Limitations

~1mm

U

5 micron tungsten sensor wire (resistance proportional to temperature)

Stainless steel prongs

Basic Single-Sensor Probe

(measures U)

See

http://www.dantecmt.com/CTA/System/probe/Single_miniature/Index.html

for real examples

U

V

Basic Two-Sensor Probe

(measures U and V)

http://www.dantecmt.com/CTA/System/probe/dual_miniature/Index.html

for real examples

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Hot-wire rake in the German-Dutch

Wind Tunnel (DNW)

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Velocity measurement

Hot-Wire Anemometry - Operation

Constant temperature operation Op Amp feedback holds wire resistance constant (and
thus temperature constant) – see the ‘golden rules’ in the Electronics Review class.
Voltage required to do this increases with velocity according to

• Dynamic response -

U

eff

E

R

1

R

2

R

3

Op Amp holds

hot wire

resistance

constant at

R

1

R

3

/R

2

Constant Temperature

Bridge (one needed

for each sensor)

See

http://www.dantecmt.com/Download/pdf_files/pi430104.pdf

for real example

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Velocity measurement

Laser Doppler Anemometer


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