Laser Doppler Anemometry Introduction to principles and applications - - PowerPoint PPT Presentation

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Laser Doppler Anemometry Introduction to principles and applications - - PowerPoint PPT Presentation

Laser Doppler Anemometry Introduction to principles and applications Contents Why measure? Characteristics and applications of LDA Principles of operation LDA fiber optical system Seeding requirements Signal characteristics


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SLIDE 1

Laser Doppler Anemometry

Introduction to principles and applications

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SLIDE 2

Contents

  • Why measure?
  • Characteristics and applications of LDA
  • Principles of operation
  • LDA fiber optical system
  • Seeding requirements
  • Signal characteristics
  • Signal processing
  • Data processing
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SLIDE 3

Why Measure?

  • Almost all industrial flows are turbulent.
  • Almost all naturally occurring flows on earth, in oceans,

and atmosphere are turbulent. Turbulent motion is 3-D, vortical, and diffusive governing Navier-Stokes equations are very hard (or impossible) to solve. Measurements are easier (easy?)

ρ ∂τ ∂ ρ ∂ ∂ Du Dt X f p X

i ij j i j

= + −

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SLIDE 4

Why Measure?

  • Industrial:

investigate technical problems check technical specs verify performance improve performance

  • Engineering:

determine parameters in turb. mode develop, extend, refine models investigate model limits

  • Theoretical

verify model predictions fluid mechanics: verify theoretical predictions verify new concepts

  • Conceptual ideas:

search for new ideas

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SLIDE 5

Characteristics of LDA

  • Invented by Yeh and Cummins in 1964
  • Velocity measurements in Fluid Dynamics (gas, liquid)
  • Up to 3 velocity components
  • Non-intrusive measurements (optical technique)
  • Absolute measurement technique (no calibration

required)

  • Very high accuracy
  • Very high spatial resolution due to small measurement

volume

  • Tracer particles are required
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SLIDE 6

Applications of LDA

  • Laminar and turbulent flows
  • Investigations on aerodynamics
  • Supersonic flows
  • Turbines, automotive etc.
  • Liquid flows
  • Surface velocity and vibration measurement
  • Hot environments (Flames, Plasma etc.)
  • Velocity of particles
  • ...... etc, etc, etc.
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SLIDE 7

LDA - Optical Principle

  • When a particle passes through the intersection volume formed by the

two coherent laser beams, the scattered light received by a detector has components from both beams.

  • The components interfere on the surface of the detector.
  • Due to changes in the difference between the optical path lengths of the

two components this interference produces pulsating light intensity as the particle moves through the measurement volume.

Photodetector

Incident beams Direction of motion Incident beams

Photodetector

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SLIDE 8

Frequency to velocity conversion

Ux

U

−K2

θ / 2

K1

ω ω ω

D D D

U k k = − = ⋅ −

1 2 1 2

r r r ( )

f U

D x

= 2 2 λ θ sin / U Cf

x D

=

C = λ θ 2 2 sin /

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SLIDE 9

LDA - Fringe Model

  • Focused Laser beams intersect and form the

measurement volume

  • Plane wave fronts: beam waist in the plane of intersection
  • Interference in the plane of intersection
  • Pattern of bright and dark stripes/planes
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SLIDE 10

Flow with particles d (known)

Velocity = distance/time

t (measured) Signal Time

Laser Bragg Cell

backscattered light measuring volume

Detector Processor

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SLIDE 11

LDA - Fringe Model

  • The fringe model

assumes as a way of visualization that the two intersecting beams form a fringe pattern of high and low intensity.

  • When the particle

traverses this fringe pattern the scattered light fluctuates in intensity with a frequency equal to the velocity of the particle divided by the fringe spacing.

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SLIDE 12

Principle of LDA, differential beam technique

Laser Signal Processing Transmitting Optics Receiving Optics with Detector Signal conditioner Flow HeNe Ar-Ion Nd:Yag Diode Beamsplitter (Freq. Shift)

  • Achrom. Lens

Gas Liquid Particle

  • Achrom. Lens

Spatial Filter Photomultiplier Photodiode Spectrum analyzer Correlator Counter, Tracker Amplifier Filter PC

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SLIDE 13

Laser, Characteristics and Requirements

  • Monochrome
  • Coherent
  • Linearly polarized
  • Low divergence

(collimator)

  • Gaussian intensity

distribution

Laser L-Diode collimator Laser

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SLIDE 14

Transmitting Optics

Basic modules:

  • Beam splitter
  • Achromatic lens

Options:

  • Frequency shift (Bragg

cell)

– low velocities – flow direction

  • Beam expanders

– reduce measurement volume – increase power density Laser Bragg Cell BS F D × E ϑ × Ε D DL Lens

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SLIDE 15

Measurement Volume

  • The transmitting system

generates the measurement volume

  • The measurement

volume has a Gaussian intensity distribution in all 3 dimensions

  • The measurement

volume is an ellipsoid

  • Dimensions/diameters δx,

δy and δz are given by the 1/e2 intensity points

F θ DL Y Z X Transmitting System Measurement Volume Intensity Distribution 1/e 2 1 δz δx δy X Z Y

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SLIDE 16

Measurement Volume

Length:

ϑ Width: Height:

  • No. of Fringes:

δ λ π θ

z L

F E D = ⎛ ⎝ ⎜ ⎞ ⎠ ⎟ 4 2 sin

δ λ π

y L

F ED = 4

δ λ π θ

x L

F ED = ⎛ ⎝ ⎜ ⎞ ⎠ ⎟ 4 2 cos N F ED

f L

= ⎛ ⎝ ⎜ ⎞ ⎠ ⎟ 8 2 tan θ π

δz δx X Z δf Fringe Separation:

δ λ θ

f =

⎛ ⎝ ⎜ ⎞ ⎠ ⎟ 2 2 sin

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SLIDE 17

Lenses Interference filtre Photomultiplier

Receiving Systems

  • Receiving Optics

– Receiving optics – Multimode fibre acting as spatial filtre – Interference filtre

  • Detector

– Photomultiplier – Photodiode

Multimode fibre

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SLIDE 18

System Configurations

Forward scatter and side scatter (off-axis)

  • Difficult to align,
  • vibration

sensitive Backscatter

  • Easy to align
  • User friendly

Receiving Optics with Detector Transmitting Optics Flow R e c e i v i n g O p t i c s w i t h D e t e c t

  • r

Flow

Laser Bragg Cell Detector

Transmitting and Receiving Optics

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SLIDE 19

Backscatter Configuration

Laser Bragg Cell Colour splitter PM PM Fibre manipulators Single mode polarisation preserving fibres Flow Back scattered light Multimode fibre Multimode fibre Interference filtres Colour splitter Single mode fibres

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SLIDE 20
  • Particles moving in either the forward or reverse direction will

produce identical signals and frequencies.

Directional Ambiguity / Frequency Shift

fmax fshift fmin f u umin umax umin umax

  • With frequency shift in one beam relative to the other, the

interference fringes appear to move at the shift frequency.

  • With frequency shifting, negative velocities can be distinguished.

no shift shift

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SLIDE 21

Frequency Shift / Bragg Cell

  • Acousto-optical Modulator
  • Bragg cell requires a signal

generator (typically: 40 MHz)

  • Frequency of laser light is

increased by the shift frequency

  • Beam correction by means
  • f additional prisms

Piezoelectric Transducer fs = 40 MHz Absorber wave front Laser ϕΒ fL fL + fS

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SLIDE 22

LDA Fibre Optical System

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SLIDE 23

LDA instrumentation from Dantec

FlowLite

  • HeNe laser
  • 1 velocity component
  • With frequency shift
  • Wide selection of accessories

FiberFlow optics / transmitter

  • Ar-Ion laser required
  • 1, 2 or 3 velocity components
  • With frequency shift
  • Wide selection of probes and

accessories

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SLIDE 24

Components on the transmitting side

Overview

  • Laser: 1D, 2D, 3D: Argon-ion: air or water cooled
  • 60X41 Transmitter
  • 60X24 Manipulators
  • FiberFlow series probe

Laser (Ar -ion) + 60X41 4 × 60X24 60X61

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SLIDE 25

The 60X41 Transmitter

The 60X41 Transmitter

  • Divides the laser beam into two:

– one direct – one frequency shifted

  • Each beam is then separated into

three colors: – green λ = 514,5 nm – blue λ = 488 nm – purple λ = 476,5 nm

  • Each color is used for measuring one velocity component. Thus the

transmitter can be used for 1D, 2D and 3D measurements.

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SLIDE 26

The 60X24 Manipulator

  • The manipulator centers and directs

the laser beam to get the maximum amount of light coupled into the thin single mode optical fibers of the fiber flow probe.

  • For each output beam from the

transmitter one 60X24 Manipulator is needed.

  • Thus, for a 3D system 6 manipulators

are needed

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SLIDE 27

A 60 mm 2D FiberFlow probe

The FiberFlow probe comprises

  • Four fiber plugs for coupling with the manipulators.
  • Four single mode fibers - one for each of the

transmitted beams - cased in an enforced cable hose.

  • One multimode fiber used as receiving fiber in

backscatter cased in the same hose.

  • The probe house.
  • One of several front lenses.

Can be used with a 55X12 Beam Expander to reduce probe volume

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SLIDE 28

The 85 mm FiberFlow probes

60X80 - 83 55X12 50X57 - 59 A B

  • The 85 mm probes provide maximum flexibility for adjustment giving large

variation in incident angle of the beams.

  • Can be used with a 55X12 Beam Expander to reduce probe volume

60X80 - 83

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SLIDE 29

Assembled FiberFlow transmitting

  • ptics

60X41 4 60X24 60X61

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SLIDE 30

60 mm and 85 mm FiberFlow probes

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SLIDE 31

FiberFlow setup for 3-D velocity measurements

  • Measuring three velocity

components requires three beam pairs. – Two pairs are emitted from a 2D probe – One pair from a 1D probe

  • The two probes are aligned so their

intersection volumes coincide.

  • The velocity components measured

by the beams from the 2D probe are

  • rthogonal.
  • The third velocity component can be
  • rthogonalized by software.
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SLIDE 32

Probe volume alignment for 3-D velocity measurements

  • To measure three velocity

components requires careful alignment.

  • The simplest method is by

using a fine pinhole with an

  • pening just large enough

that the focused beam can pass through.

  • Fine adjustment can be made

using a power meter behind the pinhole maximizing the power of light passing through the pinhole for each beam.

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SLIDE 33

The small integrated 3D FiberFlow probe

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SLIDE 34

3-D LDA Applications

  • Measurements of boundary layer separation in wind

tunnels

  • Turbulent mixing and flame investigations in combustors
  • Studies of boundary layer-wake interactions and

instabilities in turbines

  • Investigations of flow structure, heat transfer, and

instabilities in heat exchangers

  • Studies of convection and forced cooling in nuclear

reactor models

  • Measurements around ship models in towing tanks
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SLIDE 35

Seeding: ability to follow flow

ParticleFrequencyResponse d dt U d U U

p p p f p f

= − − 18

2

ν ρ ρ /

Particle Fluid Diameter (µm)

f = 1 kHz f = 10 kHz Silicone oil atmospheric air 2.6 0.8 TiO2 atmospheric air 1.3 0.4 TiO2

  • xygen plasma

3.2 0.8 (2800 K) MgO methane-air flame 2.6 0.8 (1800 K)

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SLIDE 36

Seeding: scattered light intensity

180 90 270 210 150 240 120 300 60 330 30 180 330 210 240 300 270 150 120 90 60 30 180 210 150 240 120 270 90 60 300 30 330

dp≅0.2λ

dp≅1.0λ

dp≅10λ

  • Polar plot of scattered light intensity versus scattering angle
  • The intensity is shown on a logarithmic scale
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SLIDE 37

Signal Characteristics

  • Sources of noise in the LDA signal:

– Photodetection shot noise. – Secondary electronic noise, thermal noise from preamplifier circuit – Higher order laser modes (optical noise). – Light scattered from outside the measurement volume, dirt, scratched windows, ambient light, multiple particles, etc. – Unwanted reflections (windows, lenses, mirrors, etc).

  • Goal: Select laser power, seeding, optical parameters, etc. to maximize the

SNR.

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SLIDE 38

Data Processing Specifications

What is important to know about an LDA software package?

  • What functions does it perform?

–data acquisition? –instrument control? –data processing? –graphics output?

  • What is the Input/Output?
  • How much Flexibility is there?

–ST(f)unbiased, ST(f)biased –ST(f)cov, ST(f)FFT

  • Is it EASY to use?
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SLIDE 39

Measurement of air flow around a helicopter rotor model in a wind tunnel

Photo courtesy of University of Bristol, UK

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SLIDE 40

Measurement of water flow inside a pump model

Photo courtesy of Grundfos A/S, DK

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SLIDE 41

Phase resolved and phase averaged data

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SLIDE 42

Measurement of velocity profiles in a water pipe

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SLIDE 43

Velocity profile, fully developed turbulent pipe flow

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SLIDE 44

Measurement of flow field around a 1:5 scale car model in a wind tunnel

Photo courtesy of Mercedes-Benz, Germany

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SLIDE 45

Measurement of wake flow around a ship model in a towing tank

Photo courtesy of Marin, the Netherlands

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SLIDE 46

Measurement of air flow field around a ship model in a wind tunnel

Photo courtesy of University of Bristol, UK

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SLIDE 47

Wake flow field behind hangar

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SLIDE 48

Measurement of flow around a ship propeller in a cavitation tank

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SLIDE 49

Measurement of flow in a valve model

Photo courtesy of Westsächsische Hochschule Zwickau, Germany

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SLIDE 50

Comparison of EFD and CFD results