Stroboholography for the analysis of vibration modes of mechanical systems/Mechaniniu sistemu virpesiu komponenciu analize strobo holografijos metodu.
Vasiliauskas, R. ; Palevicius, A. ; Busilas, A. 等
1. Introduction
The holographic interferometry is used in vibration and modal
analysis, structural analysis, composite materials and adhesive testing,
stress and strain evaluation, and flow, volume/shape, and thermal
analysis. All these applications derive from one or more of the four
basic methods of the applied holographic interferometry: real-time,
double exposure, time-average holography and stroboholography.
The first three holographic methods for investigating static and
dynamic processes in various mechanical, electromechanical and
microelectromechanical systems, the methodologies of the analysis of
obtained interferograms are widely described in the literature,
including [1-10]. Effectiveness of one or another method in solving
specific problems is preconditioned by several factors--the form of
analysed dynamic process (harmonic vibrations, multicomponent
vibrations, random vibration processes, impact processes, etc.) the type
of the desired information (qualitative or quantitative), conditions of
the carried out experiment. In Fig. 1 the examples of interferograms,
that are obtained using the methods of holographic
interferometry--real-time, double exposure, time-average holography--for
analysing and improving operation of the above systems and design
solutions are presented.
In Fig. 1, a, b the interferograms of piezoelectric motion
transducers obtained by the average-time method for various regimes of
operation are presented. The transducers are excited by harmonic signals
of different frequencies, so it is important to visualize the nature of
the vibrations at different time moments of the vibration period.
The reliability of computer operation largely depends on hard disc
housing deformations at different temperature regimes. The visualization
of hard disc housing deformations, qualitative and quantitative
assessment of the deformations is actual problem at development and
design phases. The presented in Fig. 1, c interferogram of hard disc is
obtained by the method of double exposure, under the changing
temperature regime.
The object shown in Fig. 1, d presents the advances in the design
of vibromotors using holographic interference methodologies [1]. The
vibromotor itself is interpreted as a mechatronic system consisting of a
piezoelectrical actuator and the driven object. The principle of design
covers the areas of the application of standing deformation wave energy
and propagating wave energy. The specifics of vibromotors are achieving
high precision levels in the motion of the driven object [11]. The only
way for increasing the accuracy levels of vibromotors is exploiting
specific geometric shapes of materials for the actuator and especially
in the contacting zones. The method of laser holographic interference is
used for determination and control of working characteristics of
vibromotors (eigenshapes at appropriate resonance frequencies transfer
of waves in the contact zones, etc.). The experimental data is later
used as source data for numerical optimization of the design methods of
vibromotors. The methods of holography interferometry are used for the
extraction of objective experimental characteristics of the working
regimes, what later gives the guidelines for optimisation of
vibromotors' design. The applied methods of laser holography have
to be different for the two working regimes. In the first case, when the
output (driven) part is motionlessly fixed, it is possible to use the
laser with continuous beam. In that case the method of realtime data
processing is used, the motion of objects is averaged in time and time
modulation is used (real-time stroboholography). That method can be
applied, as the driven part is motionless, and the processes taking
place in the contact zone between input and output links do not give
rise to longitudinal motion, and do not affect the optical
transformation. In case when the driven part is performing longitudinal
motion (each of them can differ by its character) the holography method
must use the following procedures--impulse holography with compensation
of motion of the analysed object
Vibrational dispergator (holographic interferogram of actuator is
presented in Fig. 1, e) consists of concentrically located cylinder
shaped ultrasound processing chambers [1]. The cylindrical walls of the
chambers are formed of piezoelectric actuators fed by the power sources.
When the liquid is fed into the ultrasound processing chambers and the
piezo-actuators start vibrating at their resonance frequencies, radial
standing waves are generated around each actuator. The resonance
frequency for the actuators is different and depends on radii of the
actuators. Thus the flowing liquid is processed with higher frequency
ultrasound every time it passes through the next processing ring. At the
same time the high peak constant current actuators radiate high energy
impulses to the processed liquid. Thus the whole process of dispergation
turns to be more effective. The quality regulation of the dispergation
may be performed by control of the level of constant voltage peak. It
was proven experimentally that the effectiveness of the process is
increased 3 times.
[FIGURE 1 OMITTED]
Holographic interferometry is a powerful tool for the analysis
dynamic of microelectromechanical systems [5, 8, 12 - 14]. It is a
nondestructive whole field technique capable of registering
microoscillations of MEMS components. There exist numerous methods used
for the interpretation of patterns of fringes in the holograms of
analyzed objects [15 - 17]. Unfortunately, sometimes straightforward
application of these motion reconstruction methods (fringe counting
technique, etc.) does not produce acceptable results. A typical example
is holographic analysis of a micro-electromechanical switch which is
described in [5].
The cantilever vibrations of microelectromechanical switch produce
nonlinear effects in microstructure. Holographic interferogram of
vibrating surface of such cantilever can not be evaluated
straightforward using characteristic function for distribution
interference fringes in case when time-average method for recording
hologram is used. The characteristic function of the distribution of
interference fringes of the vibrating surface should be chosen
respectively to the nature of nonlinearities taking place in working
regimes of microelectromechanical system.
A direct method to reduce the recording time during the pulsed
illumination in stroboscopic holographic interferometry is suggested.
The technique involves increasing the recording time while the object is
in static position and decreasing the recording time during the pulsed
illumination accordingly while the object is vibrating. The approach is
applied to double-exposure and triple-exposure cases of stroboscopic
holographic interferometry, where it is found that considerable
reduction in the recording time is possible.
An experimental evaluation of a stroboscopic technique as applied
to holographic interferometry is described. This technique is applicable
in the analysis of vibrations with high amplitudes and complex wave
forms and in the investigation of phase-dependent and nonsymmetrical
effects.
2. Theoretical background of the methodology
For the analysis of vibrational processes of the objects, which are
excited by harmonic and nonharmonic signals it is very important to
carry out the qualitative and quantitative analysis of vibrations
distribution on the surface within a single period [18, 19]. In this
case, it is reasonable to use the stroboholography method. The paper
presents the methodology of strobo pulse formation and synchronization
with the corresponding vibration phase, allowing to increase the
information generated by holographic interferograms and accuracy of the
analysis. In order to ensure optimal hologram exposure time (not more
than 1 to 1.5 min) and information in the obtained interferograms it is
necessary to select vibrations period filling by strobo pulses of the
lowest possible duration given by the expression of [T.sub.1]/k, where
[T.sub.1] is period of excitation signal, which depends on the analysed
object, and the value of which can be practically from 0.1 to 5 [micro]s
k is the number of strobo pulses.
[FIGURE 2 OMITTED]
In Fig. 2 the structural scheme of excitation signal formation,
strobo pulse generation and synchronization with the desired vibration
phase is presented. The signal from the generator of harmonic signals 8
or nonharmonic signal generator 12, through commutator K is transferred
to the rectangular pulse forming scheme 11. The formed rectangular pulse
signal the period of which corresponds the period [T.sub.1] of the
excitation of signal of the analysed object is fed into the pulse
splitting, counting and strobo pulse forming block 7. From this block,
the signal is input into strobo pulse commutation and separation block
10 and the excitation signal forming block 6. The separated pulse, the
duration of which may vary from 0.1 to 5 [micro]s, is formed with the
transfer characteristics ensuring the period of pulse fronts not higher
than 10-15% of the minimum strobo pulse duration by strobo pulse forming
scheme 9. Strobo pulse amplifier 5 amplifies the strobo pulse up to the
voltage needed to control electro--optical modulator.
Strobo pulse synchronization with the corresponding phase of
excitation signal is illustrated by the diagram in Fig. 3
[FIGURE 3 OMITTED]
The diagram shows the selection possibility of two strobo pulses:
the first strobo pulse corresponds the start time of excitation signal;
the second one is shifted in phase with reference to the first one. This
methodology of stobo pulse formation has a number of advantages:
* the synchronization between strobo light pulse and the vibration
phase of the analysed object is achieved throughout all the hologram
exposure time;
* several strobo pulses of the necessary duration can be used for
vibration analysis during one period of vibrations;
* strobo light pulse duration can be changed from [T.sub.1]/ up to
[T.sub.1]/k.
3. Analysis of the obtained interferograms
The case is analysed where an object, any point of the surface of
which in the direction of normal component vibrates in accordance with
the law as described by the
equation:
W (x, y, t ) = A ( x, y) sin[[omega].sub.1]t (1)
and holographic interferogram is recorded with the help of short
laser light pulses, which are synchronized with the maximum amplitude of
the vibrating surface position.
The frequency of laser beam pulses, illuminating the object and the
hologram at these moments in time is equal to the frequency of the
object vibration [f.sub.1] = [[omega].sub.1]/2[pi], while their minimum
duration is [[pi].sub.i] = [T.sub.1]/[k.sub.1], where [T.sub.1] is the
period of vibrations of the object under investigation; [k.sub.1] is the
number of rectangular pulses forming the excitation signal (filling in
the vibration period). Each of these pulses can be electrically selected
as the strobo pulse. Then the center of strobing pulse will at the time
instant [T.sub.1]/4+m [T.sub.1], where m = 0, 1, 2, 3 and the light
intensity distribution in the obtained hologram can be described by the
following equation [17]
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (2)
where [bar.I](x,y) is intensity of recovered image of point (x, y)
against the intensity at the point that during all the period of
vibrations was in zero position; [J.sub.0], [J.sub.n] are Bessel
function of the first type of order 0 and n accordingly; K is
sensitivity vector of holographic interferometer at the point (x, y)
[2]; A is amplitude of the object surface vibration at the point (x, y).
With this method of the object and hologram illumination, the
reduction of strobo pulse duration significantly reduces the influence
of the object displacements on the recovered image quality, but
significantly prolongs the duration of the hologram exposure. Assuming
[k.sub.1] = [infinity], and then sinn[pi]/[k.sub.1]/n[pi]/[k.sub.1] = 1,
light intensity distribution is:
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (3)
Taking into account [(1).sup.p] = cos p[pi] = cos 2 p [pi]/2 and
[(-1).sup.p] / i = i sin[(2p - 1) [pi]/2] and using the features of
Bessel function [17]: [J.sub.0](z) + 2 [[infinity].[summation over
(p=1)] [J.sub.2p] (z)cos 2p [pi]/2 = cos(z) and 2i[[infinity].[summation
over (p=1)][J.sub.2p-1](z)sin[(2p - 1)[pi]/2] = i sin z, finally the Eq.
(3) can be expressed as:
[bar.I] = [[absolute value of cos(KA) + i sin(KA)].sup.2] = 1 (4)
Thus, recording the hologram with the help of very short light
pulses, which are synchronized with the phase of harmonic vibrations the
influence of the object's vibrations on the intensity distribution
field of the reconstructed image is eliminated. However, with the very
short strobo pulse duration, the exposure time of the hologram
significantly increases. In order to determine the possibilities to
eliminate these shortcomings the calculation of intensity distribution
[bar.I] =f(A/[lambda]), at different values of [k.sub.1] is be made
according to formula (2), when illumination and observation directions
are perpendicular (normal) to the object's surface.
In Fig. 4 the intensity distribution graph of the function [bar.I]
= f(A/[lambda]) for various strobo pulse values is presented. It is
known that human eye does not distinguish between light-intensity
fluctuations, which are equal to or greater than 0.82. Taking this fact
into account, it is possible to set such strobo pulse duration that for
surface points of the object, vibrating with maximum amplitude the
intensity [bar.I] value is not less than 0.82. In this case, visualizing
the reconstructed hologram of vibrating object, it will not be different
from the hologram of nonvibrating object. From Fig. 3 it can be
concluded that for low amplitudes of the tested object vibrations, which
are usually investigated by the methods of holographic interferometry
the above conditions are fulfilled at very short duration strobo pulses.
Considering optimal exposure time of the hologram, informativeness of
the interferograms, parameters of electronic part the number of strobo
pulses [k.sub.1] is selected to be 20.
[FIGURE 4 OMITTED]
When surface of the object at the same time is excited by several
harmonic components, using the method of stroboholography makes it
possible to investigate the influence of separate harmonic components of
vibrations on the analysis of surface vibrations. By selecting the
duration of strobo pulses in such a way that for surface points
vibrating with a maximum amplitude [bar.I] = j(A/[lambda]) the value
would be not less than 0.82, the image of reconstructed hologram
practically will be not different from the image of nonvibrating object.
Under this conclusion the case where surface of the object at the
same time vibrates by several harmonic components [8], each
corresponding to its three-dimensional form of vibrations will be
examined. In this case, position of each surface point of the object
during the period can be described by the equation:
W (x, y, t) = [A.sub.1] (x, y) sin [[omega].sub.1]t + [A.sub.2] (x,
y)sin ([[omega].sub.2]t + [theta]) (5)
where [A.sub.1] (x,y)sin[[omega].sub.1]t and
[A.sub.2](x,y)sin([[omega].sub.2]t + [theta]) are amplitude of vibration
components of the point (x, y) the corresponding frequencies of which
are [f.sub.1] = [[omega].sub.1]/2[pi] ir [f.sub.2] = =
[[omega].sub.2]/2[pi]; [theta] is phase shift of the component.
If interferogram of such a surface is recorded by strobo pulses
with the duration of [[tau].sub.i] = [T.sub.1]/[k.sub.1] and the
frequency [f.sub.1], and synchronized with the vibrations amplitude
position of the selected component [A.sub.1](x, y)sin [[omega].sub.1]t
so taking into account the information in Fig. 4 always the strobing
pulse duration can be chosen such a one that the indicated vibration
component practically will have no influence on the image of
reconstructed interferogram. Then the approximate expression of
characteristic function, describing the intensity distribution in the
reconstructed interferogram will be conditioned only by the vibration
component [A.sub.2]sin([[omega].sub.2]t+[theta]):
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (6)
[T.sub.e] is exposure time of the hologram, [phi] is phase of the
light wave dissipated by the object's point (x, y) at the
hologram's plane. As the sensitivity vector K of holographic
interferometer at the point (x, y) is not a function of time the phase
of light wave can be expressed as [phi] = [[phi].sub.0] + +
K[A.sub.2]sin([[omega].sub.2]t+[theta]), where [theta] is phase shift of
the second harmonic component and substituding in to Eq. (6) the
following is obtained
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (7)
Expansion of the integrand expression (7) by Besel function gives:
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (8)
For the component [A.sub.2]sin([[omega].sub.2]t+[theta]) the phase
of strobo pulse will be shifted by the value 5, where 0 < 5 < 1 is
a part of the period [T.sub.2] in which the strobo pulse is located. In
this case, integral limits at the hologram exposure will be from
[delta][T.sub.2] - [[tau].sub.i]/2 up to [delta][T.sub.2] +
[[tau].sub.i]/2 and taking into account that the midpoint of strobo
pulse in case of the component [A.sub.2]sin([[omega].sub.2]t+[theta])
will correspond the random phase of vibration
[[omega].sub.2][delta][T.sub.2] and assuming the strobo pulse duration
equivalent to the hologram exposure duration during a single period
[[tau].sub.i] = [T.sub.e] the following expression is obtained:
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (9)
It is worth mentioning that the period of strobo pulses is
[T.sub.s] and in general case [T.sub.s] [not equal to] [eta][T.sub.2]
and the fact is that in dependence on the frequency ratio the value 0
< [delta] < 1 can change with each strobo pulse. The interferogram
obtained in this way will reconstruct the images captured by each strobo
pulse at the same time. Intensity distribution of the reconstructed
interferogram in this case will be described as follows:
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (10)
where j = 0,1,2 is order number of the strobo pulse. To facilitate
the analysis of the obtained expression, acounting that [J.sub.-n] =
[(-1).sup.n][J.sub.n] and rearranging the characteristic expression (10)
results in:
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (11)
From the expression of characteristic function a conclusion can be
made that applying the proposed method of strobo pulse formation and
synchronization with the necessary vibration phase, the intensity of the
reconstructed image described by this function depends on duration of
the strobo light pulse and on the ratio of parameters of different
vibration components.
Let us analyse Eq. (12) when frequency ratio of vibration
components is irrational number. Recalling the fact--if [f.sub.2] >
[f.sub.1] and [f.sub.2]/ [f.sub.1] = q+[delta], where q = 1, 2, 3, ...,
0 < [delta] < 1 the strobo pulses during exposure time will be
repeated with the period [T.sub.1] = [T.sub.2](q+[delta]). Evaluating
all the facts above and changing summation with respect to [delta] in
expression (11) by integration will give:
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (12)
[FIGURE 5 OMITTED]
Thus when frequency ratio of the vibration components is irrational
number the proposed methodology ensures visualization of time averaged
interferogram of vibration form for one of the vibration components of
the tested object. Fig. 5 presents an example of the obtained result for
a tested plate natural frequencies of which are equal to 379 Hz and
2381.3 Hz.
Fig. 5 presents separation of the plate's vibration forms
which correspond two vibration components of different frequencies when
the ratio of vibration frequencies is irrational number: a, b -
interferograms obtained by time average method representing vibration
forms of the plate at [f.sub.1] = 379.0 Hz and [f.sub.2] =2381.3 Hz; c -
interferogram of vibration form of the plate obtained by time average
method when the plate simultaneously vibrates at the two frequencies
[f.sub.1] = 379.0 Hz and [f.sub.2] =2381.3 Hz; d - interferogram of the
plate's vibration form corresponding the vibration component the
frequency of which is [f.sub.2] when the plate simultaneously vibrates
at the two frequencies [f.sub.1] = = 379.0 Hz and [f.sub.2] = 2381.3 Hz
obtained by the method of strobo holography.
Let us analyse equation (12) when frequency ratio of vibration
components is rational number. It is assumed that [f.sub.2] >
[f.sub.1] and [f.sub.2]/ [f.sub.1] = q, where q = 2,3, .... In this case
period [T.sub.2] of the component with the frequency [f.sub.2] will be
covered within the period [T.sub.1] so that [T.sub.1]/[T.sub.2] = q is a
whole number and in this case strobo pulse duration for the component
with the frequency [f.sub.2] per period will be - [[tau].sub.i2] =
[T.sub.2]/[k.sup.1] = [T.sub.1]/q[k.sub.1]. Total time of hologram
expose in this case will be n[[tau].sub.i2]. Intensity distribution of
the recovered hologram in such a case is described by Eq. (8) which
after evaluation of strobo pulse duration, total exposure time of the
hologram and making the necessary rearrangements will take the same form
as Eq. (12). It is obvious that this expression will be correct only I
case when the number of strobo pulses during hologram exposure time is
significantly greater that the frequency ratio q of the vibration
components. Fig. 6 presents an example of the obtained result when a
plate natural frequencies of which are equal to 379 Hz and 2381.3 Hz was
tested.
[FIGURE 6 OMITTED]
Fig. 6 presents separation of the plate's vibration forms
which correspond two vibration components of different frequencies when
the ratio of vibration frequencies ([f.sub.2]/[f.sub.1] = 10) is
rational number. a, b - Interferograms obtained by time average method
representing the plate's vibration forms at [f.sub.1] = 764 Hz and
[f.sub.2] = 7640 Hz; c - interferogram of vibration form of the plate
obtained by time average method when the plate simultaneously vibrates
at the two frequencies [f.sub.1] = 764 Hz and [f.sub.2] = 7640 Hz; d -
interferogram of the plate's vibration form corresponding the
vibration component the frequency of which is [f.sub.2] when the plate
simultaneously vibrates at the two frequencies [f.sub.1] = = 764 Hz and
[f.sub.2] = 7640 Hz obtained by the method of strobo holography.
4. Concluding remarks
1. The methodology of strobo light pulses formation allowing one or
several light pulses to separate and synchronize with the phase of
excitation signal of the tested object in one period of its vibration
during the whole duration of the hologram exposure is presented.
2. For the analysis of vibrations several strobo pulses during one
period of the vibration can be used and duration of the strobo light
pulse can be practically changed from [T.sub.1]/2 up to
[T.sub.1]/[k.sub.1].
3. The methodology of component separation of 3D vibration with two
different frequency components is theoretically proven for the cases of
various frequency ratios of the components.
Received October 06, 2010
Accepted January 28, 2011
References
[1.] Palevicius, A.; Ragulskis, K.; Vasiliauskas, R.; Bubulis, A.
2008. Historical aspects and future perspective of holography in
Lithuania. The Society for Experimental Mechanics. Proceedings of the
International Symposium to Commemorate the 60th Anniversary of the
Invention of Holography. Sheraton Springfield Monach Place Hotel,
Springfield, Massachusetts USA, October 27-29: 368-377.
[2.] Palevicius, A.; Vasiliauskas, R. 1998. Application of laser
interferometry and holographic methods for analysis and design of
vibrational systems. Virpesiu mechanika ir technika. Vibroengineering:
monografija. Lietuvos Mokslu akademija. -Vilnius: Lietuvos mokslas, kn.
19: 358-381.
[3.] Vasiliauskas, R.; Palevicius, A.; Ragulskis, K. 1988. Analysis
of holographic interferograms by ultrasonic piezoelectric transducers in
the investigation of three-dimensional vibrations, Acoustical Physics
34(6): 573-575.
[4.] Patasiene, L.; Vasiliauskas, R.; Fedaravicius, A. 2005.
Application of holographic interferometry methods for anal;ysis
piezdrives with ring actuators, Ultragarsas 3(56): 17-21.
[5.] Ostasevicius, V.; Palevicius, A.; Daugela, A; Ragulskis, M.;
Palevicius, R. 2004. Holographic imaging technique for characterization
of MEMS switch dynamics. Proc. SPIE Vol. 5389, Smart Structures and
Materials 2004: Smart Electronics, MEMS, BioMEMS, and Nanotechnology;
Vijay K. Varadan; Ed.: 73-84.
[6.] Patasiene, L.; Vasiliauskas, R.; Fedaravicius, A. 2007.
Holgraphic interferometry method for determination of layer piezostack
parameters, Ultragarsas 1(6)2: 23-25.
[7.] Palevicius, A.; Busilas, A.; Vasiliauskas, R. 2008. Analysis
holographic interferogram of links of vibrating systems, Journal of
Vibroengineering (Vibromechanika), 2008 June. -Vilnius, Lithuania,
volume 10, ISSUE 2, numbers of publications from 348 to 370: 245-250.
[8.] Vasiliauskas, R.; Palevicius, A. 2008. Analysis of holographic
interferometry of microelectromechanical system with non harmonic cycles
excitation, Journal of Vibroengineering (Vibromechanika), January/March.
Vilnius, Lithuania, vol. 10 ISSUE 1, numbers of publications from 326 to
347: 42-46.
[9.] Patasien?, L.; Federavicius, A.; Vasiliauskas, R. 2008.
Holographic interferometry methods for analysis and design of rotary
converter, Journal of Vibroengineering (Vibromechanika), January/March.
-Vilnius, Lithuania, vol. 10, ISSUE 1, numbers of publications from 326
to 347: 33-36.
[10.] Ragulskis, K.; Dabkevicius, A.; Kibirkstis, E.; Bivainis, V.;
Miliunas, V.; Ragulskis, L. 2009. Investigation of vibrations of a
multilayered polymeric film, Mechanika 6(80): 30-36.
[11.] Mazeika, D.; Bansevicius, R. 2009. Study of resonant
vibrations shapes of the beam type piezoelectric actuator with preloaded
mass, Mechanika 2(76): 33-37.
[12.] Tonin, R.; Bies, D.A. 1978. Time-average holography for the
study of three-dimentional vibrations, Journal of sound and vibrations
52: 315.
[13.] Vikram, C.S. 1974. Stroboscopic holographic interferometry of
vibration simultaneously in two sinusoidal modes, Optics communications,
v.II, Nr.4: 360-364.
[14.] Shajenko, P.; Johnson, C.D. 1968. Stroboscopic holographic
interferometry, Appl. Phys. Lett. 13(1): 4446.
[15.] Harris, J.S.; Fusek, R.L.; Marcheski, J.S. 1979. Stroboscopic
interferometer, Appl. Opt. 18: 2368-2371.
[16.] Zarucki, MA.; Gurevich, V.S. 1986. On research of vibration
characteristics of the parts with stress concentrators by the method of
stroboholography. In textbook: Stress Concentration in the Elements of
Aviation Engines. Inter university research materials. Ufa aviation
Institute of S. Ordzonikidze: 97-100 (in Russian).
[17.] Vest, Ch. 1982. Holographic interferometry. Editor in chief
J.S. Ostrovski. Moscow: Mir. 504p. (in Russian)
[18.] Lee, Y-S.; Kim, S-H.; Skibniewaki, M.J. 2009. Analytical and
experimental approach for assessing vibration serviceability of highway
bridges due to heavy vehicle traffic, The Baltic Journal of Road and
Bridge Engineering 4(3): 123-133.
[19.] Bayraktar, A.; Birinci, F.; Altunisik, A.C.; Turker, T.;
Sevim, B. 2009. Finite element model updating of Senyuva historical arch
bridge using ambient vibration tests, The Baltic Journal of Road and
Bridge Engineering 4(4): 177-185.
R. Vasiliauskas, Mykolas Romeris University, Kaunas Faculty of
Public Security, V. Putvinskio 70, 44211 Kaunas, Lithuania, E-mail:
r.vasiliauskas@mruni.lt
A. Palevicius, Kaunas University of Technology, Mickeviciaus 37,
44244 Kaunas, Lithuania, E-mail: arvydas.palevicius@ktu.lt
A. Busilas, Vilnius Gediminas Technical University, Sauletekio al.
11, 10223 Vilnius, Lithuania, E-mail: alfredas.busilas@gama.vtu.lt
K. Pilkauskas, Kaunas University of Technology, Mickeviciaus 37,
44244 Kaunas, Lithuania, E-mail: kestutis.pilkauskas@ktu.lt