Article citation information:
Štalmach,
O., Dekýš, V., Novák, P., Sapieta, M. Processing
of results from a thermal FEM analysis using the lock-in method and comparison
with experiment. Scientific Journal of
Silesian University of Technology. Series Transport. 2019, 104, 159-168. ISSN: 0209-3324. DOI: https://doi.org/10.20858/sjsutst.2019.104.14.
Ondrej ŠTALMACH[1],
Vladimír DEKÝŠ[2],
Pavol NOVÁK[3],
Milan SAPIETA[4]
PROCESSING OF RESULTS FROM A THERMAL FEM ANALYSIS USING THE LOCK-IN METHOD
AND COMPARISON WITH EXPERIMENT
Summary. This
article dealt with the comparison of results obtained from an experiment and
from the numerical thermal FEM analysis. Sample with defects were printed on a
3D printer. A thermal wave from the halogen lamp to excite the front surface of
the sample was used in the next step and the response was measured by a thermal
camera. After processing the data in the software DisplayIMG, a phase image was
created representing the 2D image of the material at a certain depth under the
surface of the model. Lock-in method was applied to the results from the
numerical thermal FEM analysis and the phase image was created. The programs
code were created in MATLAB for a 4 points, multiple points and differential
lock-in method which were compared with the results from the experiment.
Keywords: lock-in method, thermal FEM analysis,
thermography, thermal excitation
1. INTRODUCTION
With the
greater availability and rapid decline in the prices of thermal cameras in the
last years, thermography has developed from being a rarely used technique to an
increasingly popular investigation method. There are a number of techniques for
evaluating the time dependence of temperature distribution.
Experimental
methods often utilise the detection of a test object's response to excitation.
An infrared camera (IRC) can also be used as a detector for these measurements.
Using a camera in the 3-5 um (MWIR) wavelength range with an InSb detector, it
is possible to detect events with microsecond integration times. This can be
used to detect the occurrence of fast events, for example, Lüders bands
[1-3], when synchronizing the camera with exciting harmonic loading events,
which is useful in thermoelastic analysis (TSA) [4,5], in determining the
dissipative energy estimation in fatigue tests [6,7,8], determining crack size
[9], in the analysis of vibration and determination of resonance frequencies
and modal shapes [10,11].
In
thermoelastic analysis, the temperature change during the adiabatic loading
cycle (when the minimum frequency for steel is 2 Hz, for Al alloys 20 Hz) is
usually very low at the ICR noise level. Increase in signal-to-noise ratio is
achieved by lock-in technology [12] processing the camera output. This
increases the sensitivity by at least 1 order, which is sufficient for determining
temperature change. In the elastic region, based on the linear relationship
between the temperature change and the trace of stress tensor, it is possible
to determine the distribution of the sum of the principal stresses on the test
object [13].
In cyclic
loading, if there is only microplastic deformation below the fatigue limit, the
radiation level corresponding to the dissipated energy of the detected IRC is
approximately constant and is a linear function of the mean and load
amplitudes. When the load is higher than the limit, this energy increases,
which is detectable by the camera. The breakpoint determines the fatigue limit
and the energy corresponding to the linear dependencies (before and after the
breakpoint) and the Wöhler curve can also be determined [14]. Such a test
is an accelerated fatigue test with loading in blocks of increasing mean and
amplitude, with the radiated energy rate determined in each block. This also
makes it possible to analyse the formation and propagation of the plastic region
in the crack root [15,16].
The
application of the MWIR IRC is significant in non-destructive testing (NDT)
when the excitation is realised, for example, cyclic loading (fatigue testing
machine), sonotrode (ultrasound) and temperature waves (halogen reflector).
Response is detected by IRC using lock-in. The output is interpreted as the
amplitude and phase of the Fourier series at lock-in frequency corresponding to
the excitation frequency [12]. Through the phase change, the defects in the
object are detectable. The excitation frequency determines the depth of defect
below the surface [17].
A separate
issue is a multi-parametric approach, where temperature dependence measurement
is also used to assess the reliability of the technology [18-25].
While the steady-state
thermography is often called "passive thermography", the techniques
evaluating dynamic temperature are called "active thermography",
since the sample temperature is actively influenced by certain means. The most
prominent examples of this class of non-steady-state or dynamic thermography
are the pulse and lock-in thermography.
2. LOCK-IN METHOD
The
lock-in principle is the technique of choice, if signals have to be extracted
from statistical noise. Prerequisite to using this technique is that the
primary signal, can be periodically pulsed or anyhow else amplitude-modulated
with a certain frequency called “lock-in frequency” flock-in [12]. The
lock-in method uses the non-destructive testing by infrared thermography to
detect the hidden defects in the sample. In this case, it is necessary to
synchronise the modulated signal of the heat source with measured data.
Moreover, the lock-in method is used, for example, in mechanics, in determining
deformation fields, or for determining the fatigue limit.
Lock-in
method can be described as a multiplication of detected signal F by a weighting factor K. This process is usually called
lock-in correlation procedure. Output signal S for synchronous correlation is obtained by linear averaging over n lock-in periods (L is phase position, N is
number of frames in one period):
The correlation function optimum to
achieve the best signal to noise ratio is the harmonic function. When we use
sine wave with amplitude A and its
phase
And weight
factors are:
Using the addition theorem of equation
(2) and equations (3) and (4) the results of correlation are [18]:
Then, the
amplitude a the phase are [9,10]:
3. EXPERIMENT
One of the
purposes of this paper is to design a 3D model with the defects (Fig. 1) that is printed on a 3D printer (Mark Two). The
defects are designed like blind holes 10x10 mm with the square cross section
with the different depth under the surface the model. The samples are printed
from the material “Onyx” which is defined by the producer as nylon mixed with chopped carbon
fibre. The macroscopic properties of the composite materials are converted from
the material properties of the components by homogenisation techniques, for
example, in this case, are taken the parameters of the basic material because
the manufacturer did not provide sufficient documentation. The thermal
properties of the Onyx are:
·
density ρ
= 1.18 g/cm3
·
isotropic thermal conductivity κ = 0.23 W/(m.K)
·
specific heat cp = 1510 J/(kg.K)
Fig. 1. 3D model with the defects
Experiment
is done using the optical excited lock in thermography and the goal is for
detection of defects in the specific depth under the surface. The basic idea of
lock-in thermography (Fig. 2) is the visualisation of thermal wave propagation.
The phase angle of such waves provides information about thermal structures and
inhomogeneities. The thermal waves are generated by intensity-modulated halogen
lamps which heat up the surface. The signal is captured by a high-resolution
infrared camera. The evaluation method “R/L-Algorithm” allows for
the determination of thicknesses and thermal reflection coefficients. A
sinusoidal thermal source is used to excite the surface of a sample. The
thermal excitation source consisted of one halogen lamp of 2.5 kW, driven by a
power amplifier and a function generator.
In addition to optical excitation, which is considered
optimal for composites, other types are also used, such as ultrasonic
excitation of metallic materials.
For detection of thermal waves, a thermal camera FLIR SC7500
with cooled detector was used. This IR camera has a temperature resolution of
20 mK and 320 x 256 pixel resolution. The camera is attached to the thermal
source, which is used to generate harmonic waves passing the sample with
adequate frequency. The thermal camera frame rate is set to 100 frames per
second.
In the DisplayIMG software, measured data from the thermal
camera are processed using the lock-in method and the result is the phase
image. Lock in frequency is used to determine reaction at certain depth
Fig.
2. Principle of optically excited Lock-in thermography
Lock-in frequency is same as the frequency of the stimulated
thermal wave. In this experiment,the lock-in frequency was set to 0.1719 Hz
which represents the reaction from the depth around 0.5 mm under the surface.
Configuration of devices which were used in the experiment is shown in Fig.
3a). The phase image which was getted from the DisplayING was imported to
Matlab and a 176 x 176 image is cropped from the 320 x 256 image showing only
samples without the other background (Fig. 3b).
4. NUMERICAL FEM SIMULATIONS
Sample
with the defects (Fig. 1) is stimulated by the heat flux with the cosines
amplitude in the program Ansys workbench. This thermal simulation represented
an experiment in which the model is stimulated by the heat flux using the
halogen lamp. On the front surface of the model is applied the heat flux M, which represent the thermal wave used
in the experiment. Maximum of the heat flux amplitude is 12.8 W/m2
which is computed from the data of power of the halogen lamp used in the
experiment. Cosine wave of the heat flux is applied using the data in Tab. 1.
On the other surfaces of the sample is applied the convection which represents
a natural heat transfer between the object and the ambient air and its value is
20 W/m2.K.
Fig.
3. Configuration of the devices (a), and phase image from the experiment (b)
Tab.
1
Values of the heat flux M across the time t
|
1. |
2. |
3. |
4. |
5. |
6. |
7. |
8. |
9. |
10. |
t [s] |
0 |
0.646 |
1.292 |
1.939 |
2.585 |
3.231 |
3.878 |
4.524 |
5.171 |
5.817 |
M [W/m2] |
0 |
1.497 |
5.288 |
9.6 |
12.414 |
12.414 |
9.6 |
5.288 |
1.497 |
0 |
On
the front surface of the numerical model of the sample was created the mapped
mesh 176 x 176 nodes, which represent the 176 x 176 pixels of the thermal
camera covering the surface of the sample. The final numerical mesh contained 635
072 nodes, 133 125 elements and was made up of the hexahedral linear elements. The boundary conditions are shown in
Fig. 4.
After
the simulations, the nodes on the front surface (176 x 176) and its values of
the temperature were exported to the text file. It is done for the every time
step from the Tab. 1. From these text files were created 2D matrices, which
represent the distribution of the temperature on the front surface of the
sample. It is similar to the image created by the thermal camera. After processing
these images using the lock-in method, the phase images were created. Three methods of lock-in were used:
·
four points lock-in method which uses only
the four images at the position 2, 4, 6, 8 (Fig. 5a)
·
multiple points lock-in method which uses all
the images (Fig. 5b)
·
differential lock-in method which on the
beginning subtract the first image from the others than is calculated from this
differential images (Fig. 5c)
Fig.
4. Front surface (blue) and the others
Fig.
5. Four points lock-in (a), multiple points lock-in (b), and differential
lock-in (c)
The phase images look identical like the phase image from the
experiment. To determine the deviations of these three results from the
measured result of the experiment, it is necessary to select a line (profile)
from all of these phase images that are on the y-axis at the position 40 (red
arrow). These lines are after that normalise because of comparison on the same
scale. The
results are shown in Fig. 6.
Fig. 6. Four points lock-in vs. experiment (a), multiple points lock-in
vs. experiment (b), and differential lock-in vs. experiment (c)
In
the table are shown the percentage differences between the three peaks of the
line from the experiment and from the numerical simulation.
Tab. 2
Differences
between the lines
|
Experiment
|
Numerical simulation (red line) |
Absolute differences |
Peak a) (Left) |
2.46 |
2.05 |
0.41 |
Peak
a) (Middle) |
0.55 |
1.15 |
0.6 |
Peak
a) (Right) |
-
0.22 |
0.45 |
0.67 |
Peak
b) (Left) |
2.46 |
2.46 |
0 |
Peak
b) (Middle) |
0.55 |
0.46 |
0.09 |
Peak
b) (Right) |
-
0.22 |
-
0.17 |
0.05 |
Peak
c) (Left) |
2.46 |
1.72 |
0.74 |
Peak
c) (Middle) |
0.55 |
1.47 |
0.92 |
Peak c) (Right) |
-
0.22 |
0.59 |
0.81 |
From
these results, it is obvious that the multiple points lock-in method is closest
to the experiment. This is because the software DisplayIMG also uses this
method to process data from the infrared camera. This method is the closest to
reality because when the lock-in frequency 0.1719 Hz is used to represent the reaction from the depth around 0.5 mm
under the surface, only the first two defects were seen.
5. CONCLUSION
In
this article, the sample with defects was printed on a 3D printer and was used
for the optical lock-in thermography. Also using this model, the numerical FEM
simulation representing this optical lock-in thermography was created. A
sinusoidal thermal source (halogen lamp) was used to excite the surface of the
sample and a thermal camera FLIR SC7500
was used for detection. The phase image was getted
from the DisplayING. Phase image representing the 2D image of the
material at a depth 0.5 mm (because lock-in frequency is 0.1719 Hz) under the
surface of the model. After processing, the data from the experiment and
numerical simulation was created. In MATLAB, was created programs for 4 points,
multiple points and differential lock-in method, which were used to process
data from the numerical simulation. These methods were compared to the
experiment. The multiple points lock-in method is the closest to the experiment
and reality. Therefore, this method can be used in future research.
Acknowledgements
This paper
was supported by KEGA 017ŽU-4/2017 and by the Slovak Research and
Development Agency under contract No. APVV–0736–12.
References
1.
Louche Hervé, André Chrysochoos. 2001. „Thermal and dissipative
effects accompanying Lüders band propagation”. Materials Science and Engineering 307(1-2): 15-22. ISSN 0921-5093.
DOI: https://doi.org/10.1016/S0921-5093(00)01975-4.
2.
Srinivasan Nagarajan, N. Raghu,
Balasubramanian Venkatraman. 2012. “Study on lüders deformation in
welded mild steel using infrared thermography and digital image
correlation”. Advanced Materials
Research 585: 82-86. ISSN 1662-8985. DOI: https://doi.org/10.4028/www.scientific.net/AMR.585.82.
3.
Brlić Tin, Stoja Rešković, Ivan
Jandrlić, Filip Skender. 2018. „Influence of strain rate on stress
changes during Lüders bands formationand propagation”. IOP Conference Series: Materials Science and
Engineering 461(1): 012007. ISSN: 1757-899X. DOI:
doi:10.1088/1757-899X/461/1/012007.
4.
Chandraprakash Chindam, Chitti Venkata Krishnamurthy,
Krishnan Balasubramaniam. 2019. „Thermomechanical phenomenon: a
non-destructive evaluation perspective”. Transactions of the Indian Institute of Metals: 1-11. ISSN 0975-1645. DOI:
https://doi.org/10.1007/s12666-019-01656-6.
5.
Patterson Eann A., Robert E. Rowlands. 2008.
„Determining individual stresses thermoelastically”. The Journal of
Strain Analysis for Engineering Design 43(6): 519-527. ISSN
0309-3247. DOI: https://doi.org/10.1243/03093247JSA358.
6.
Fargione Giovanna, Alberto Geraci, Guido La Rosa,
Antonino Risitano. 2002. „Rapied determination of the fatigue curve by
the thermographic method”. International
Journal of Fatigue 24(1): 11-19. ISSN 0142-1123. DOI:
10.1016/S0142-1123(01)00107-4.
7.
De Finis Rosa, Davide Palumbo, Francesco Ancona, Umberto Galietti. 2015.
„Fatigue limit evaluation of various martensitic stainless steels with
new robust thermographic data analysis”. International Journal of Fatigue 74: 88-96. ISSN 0142-1123. DOI: https://doi.org/10.1016/j.ijfatigue.2014.12.010.
8.
Sága, Milan, Peter Kopas, Milan
Uhríčik. 2012. „Modeling and experimental analysis of the
aluminium alloy fatigue damage in the case of bending - torsion loading”.
Procedia Engineering 48: 599-606. ISSN 1877-7058. DOI: https://doi.org/10.1016/j.proeng.2012.09.559.
9.
Ju Shen-Haw, Robert E. Rowlands. 2007.
“Thermoelastic determination of crack-tip coordinates in
composites”. International Journal
of Solid and Structures 44 (14-15): 4845-4859. ISSN 0020-7683. DOI: https://doi.org/10.1016/j.ijsolstr.2006.12.003.
10.
Montanini Roberto, Fabrizio Freni. 2013.
„Correlation between vibrational mode shapes and viscoelastic heat
generation in vibrothermography”. NDT & E International 58: 43-48.
ISSN 0963-8695. DOI: https://doi.org/10.1016/j.ndteint.2013.04.007.
11.
Sága Milan, Róbert Bednár, Milan
Vaško. 2011. „Contribution to modal and spectral interval finite
element analysis”. In: Vibration
Problems ICOVP 2011 Springer Proceedings in Physics 139, edited by
Jiŕí Náprstek, Jaromír Horáček,
Miloslav Okrouhlík, Bohdana Marvalová, Ferdinand Verhulst,
Jerzy T. Sawicki, 269-274. Springer, Dordrecht.
ISBN 978-94-007-2069-5. DOI: https://doi.org/10.1007/978-94-007-2069-5_37.
12.
Breitenstein Otwin, Warta Wilhelm, Langenkamp Martin.
2010. Lock-in thermography. Springer
Series in Advanced Microelectronics. 2. Edition. ISBN 978-3-642-02416-0.
13.
Dulieu-Barton Janice M. 1999. „Introduction to
thermoelastic stress analysis”. Strain 35(2):
35-40. ISSN 0039-2103. DOI: https://doi.org/10.1111/j.1475-1305.1999.tb01123.x.
14.
Micone Nahuel, Wim De Waele. 2017.
„On the application of infrared thermography and potential drop for the
accelerated determination of an S-N Curve”. Experimental Mechanics 57(1): 143-153. ISSN 0014-4851. DOI: https://doi.org/10.1007/s11340-016-0194-6.
15.
Jones Rhys, Susane Pitt. 2006. „An experimental
evaluation of crack face energy dissipation”. International Journal of Fatigue 28(12): 1716-1724. ISSN
0142-1123. DOI: https://doi.org/10.1016/j.ijfatigue.2006.01.009.
16.
Pottier Thomas, Franck Toussaint, Hervé Louche, Pierre Vacher. 2013. „Inelastic heat
fraction estimation from two successive mechanical and thermal analyses and
full-field measurements”. European Journal of Mechanics - A/Solids 38: 1-11. ISSN:
0997-7538. DOI: https://doi.org/10.1016/j.euromechsol.2012.09.002.
17.
Vavilov Vladimir. 2009. „Thermal / Infrared
testing”. In Nondestructive testing,
edited by Klyuev Vitaly V, 11-452. Volume 5. Book 1. Russia: Spektr, ISBN
978-8-904270-01-8.
18.
Kekez Michal, Leszek
Radziszewski, Leszek,
Alzbeta Sapietova. 2015. „Fuel type recognition by classifiers developed with computational
intelligence methods using combustion pressure data and the crankshaft angle at
which heat release reaches its maximum”. Procedia Engineering 136: 353-358. ISSN 1877 7058. DOI: https://doi.org/10.1016/j.proeng.2016.01.222.
19.
Žuľová Lucia, Robert Grega, Jozef Krajňák,
Gabriel Fedorko, Vieroslav Molnár. 2017. “Optimization of
noisiness of mechanical system by using a pneumatic tuner during a failure of
piston machine”. Engineering
Failure Analysis 79: 845-851. ISSN 1350-6307.
20.
Sapietova Alzbeta,
Milan Saga, Ivan Kuric, Stefan Vaclav. 2018. „Application of optimization algorithms for robot systems
designing“. International
Journal of Advanced Robotic Systems 15(1): 1729881417754152.
ISSN 1729-8814. DOI: https://doi.org/10.1177/1729881417754152.
21.
Bakowski Andrzej,
Michal Kekez, Leszek Radziszewski, Alzbeta Sapietova.
2018. „Vibroacoustic real time fuel classification in diesel engine“. Archives of Acoustics
43(3): 385-395. ISSN 0137-5075. DOI: 10.24425/123910.
22.
Homišin J., R. Grega, P. Kaššay, G. Fedorko, V. Molnár.
2019. “Removal of systematic failure of belt conveyor drive by reducing
vibrations”. Engineering Failure
Analysis 99: 192-202. ISSN 1350-6307.
23.
Grega, R., J. Krajňák, L. Žuľová, G. Fedorko,
V. Molnár. 2017. “Failure analysis of driveshaft of truck body
caused by vibrations”. Engineering
Failure Analysis 79: 208-215. ISSN 1350-6307.
24.
Maldague Xavier, P.V., Moore Patric O. 2001. Nondestructive testing handbook: infrared and thermal
testing. 3. Edition. Amer Society for Nondestructive. ISBN:
1-57117-044-8.
25.
Urbanský M., J. Homišin, P.
Kaššay, M. Moravič. 2016. “Influence of piston compressor
inner failure on mechanical system objective function”. Diagnostyka 17(3): 47-52. ISSN
1641-6414.
Received 17.05.2019;
accepted in revised form 17.08.2019
Scientific Journal of Silesian University of
Technology. Series Transport is licensed under a Creative Commons Attribution
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[1]
Faculty of Mechanical Engineering, University of Zilina, Univerzitná 1,
010 26 Žilina, Slovakia. Email: ondrej.stalmach@fstroj.uniza.sk
[2]
Faculty of Mechanical Engineering, University of Zilina, Univerzitná 1,
010 26 Žilina, Slovakia. Email: ondrej.stalmach@fstroj.uniza.sk
[3]
Faculty of Mechanical Engineering, University of Zilina, Univerzitná 1,
010 26 Žilina, Slovakia. Email: ondrej.stalmach@fstroj.uniza.sk
[4]
Faculty of Mechanical Engineering, University of Zilina, Univerzitná 1,
010 26 Žilina, Slovakia. Email: ondrej.stalmach@fstroj.uniza.sk