Damage Identification of the Sandwich Plate Having Core from Rice
Husk-Epoxy for Ship Deck Structure
Abdi Ismail
1
, Achmad Zubaydi
1
, Agung Budipriyanto
2
and Yudiono
1
1
Department of Naval Architecture, Faculty of Marine Technology, Institut Teknologi Sepuluh Nopember (ITS), Jl. Arief
Rahman Hakim, Surabaya, Indonesia
2
Department of Civil Infrastructure Engineering, Faculty of Vocational Studies, Institut Teknologi Sepuluh Nopember (ITS),
Jl. Menur 127, Surabaya, Indonesia
Keywords: Ships Structure, Sandwich Plate, Damage Identification, Natural Frequency, Ramping Ratio.
Abstract: This paper discusses vibration-based damage identification applied on sandwich plate for ship structure using
Finite Element Analysis Method (FEM) and Experimental Modal Analysis (EMA). The sandwich plate had
6mm-thick steel faceplates and 15mm-thick core. The core was made from epoxy and rice husk powder with
two compositions, i.e., 10% and 15% rice husk powder by weight. The thickness of the faceplates and the
core was designed for the main deck of a coal barge ship. Damage was introduced in the core. Then natural
frequency and damping were measured before and after the damage was introduced. It was observed that for
the sandwich plate with core made from 10% rice husk, the natural frequency deviations due to damage
obtained by EMA and FEM is 0.39% and 0.81% respectively. Natural frequency deviations obtained by EMA
and FEM for the sandwich with the core of 15% rice husk is 5.39% and 5.00% respectively. The damping
ratios deviations due to damage for sandwich with core of 10% and 15% rice husk powder differed by 0.16%
and 0.13% respectively. Thus, natural frequency and damping ratio could be used as damage identification
parameters. Nevertheless, sensitivity analysis of the damage size is required for future development.
1 INTRODUCTION
The use of sandwich plate in ship structures has
several advantages. The weight of the structure using
sandwich plate is lighter than the that of conventional
stiffened plate structure. It was reported that the
weight reduction was more than 10% (Momčilović &
Motok, 2009). Another advantage is better
construction design and easier fabrication process
(Ramakrishnan & Kumar, 2016).
The sandwich plate can be fast constructed. It has
high stiffness-weight ratio, high fatigue strength,
good acoustic and thermal insulation (Reis &
Rizkalla, 2008). The sandwich plate consists of two
parts, the faceplates and the core. The faceplate is
made of material that has high strength and stiffness
while the core layer is made of materials that has
lower strength, stiffness and material density
(Borsellino, et al., 2004). The combination of the two
parts will provide a very efficient strength-weight
ratio, which is a key requirement for lightweight
structures such as those used in the shipping industry.
The use of sandwich plate on the ship's structure
would reduce the overall weight of the ship so that it
could increase the payload.
Several studies of sandwich plate applications on
ships have been carried out. Research on the design
and testing of T-joint sandwich for ships has been
carried out (Toftegaard & Lystrup, 2005). Sandwich
made of faceplate steel and concrete cores have been
researched for ship hull applications (Dai & Liew,
2006). In the maritime field, sandwich plate have
potential applications in bridge decks, anti-collision
structures, ship hulls and offshore structures (Liew &
Sohel, 2009). Sandwich Plate System (SPS) has been
applied to ship repair using an overlay process
(Momčilović & Motok, 2009). Research on the peak
strength of L-joint sandwich for ship structures was
carried out (Shen, et al., 2017).
Ships structure needs the Structural Health
Monitoring (SHM) and damage identification to
prevent catastrophic structural failure. SHM will be
developed based on the damage identification
method. Local damage-identification methods are
difficult to do on large structures, complex structures,
or structures that are difficult to access (Yan, et al.,
112
Ismail, A., Zubaydi, A., Budipriyanto, A. and Yudiono, .
Damage Identification of the Sandwich Plate Having Core from Rice Husk-Epoxy for Ship Deck Structure.
DOI: 10.5220/0008543301120118
In Proceedings of the 3rd International Conference on Marine Technology (SENTA 2018), pages 112-118
ISBN: 978-989-758-436-7
Copyright
c
2020 by SCITEPRESS – Science and Technology Publications, Lda. All rights reserved
2007), as in ship structures. Global damage-
identification such as vibration method is an effective
and appropriate way to detect damage in large and
complex ship structures.
Global damage-identification using vibration
method has been conducted by many researchers. All
structures can be expressed as dynamic systems with
certain structural parameters, such as stiffness, mass,
and damping constants. If the structure gets damaged,
the structural parameters will also change (Yan, et al.,
2007). Thus, changes in these structural parameters
can be detected through vibration signals that indicate
the existence of damage in a structural system (Shi, et
al., 2000; Gawronski & Sawicki, 2000; Kawiecki,
2001; Shi, et al., 2002; Abdo & Hori, 2002; Sampaio,
et al., 2003; Fan & Qiao, 2011). Vibration method
detects the existence of damage in certain objects by
observing changes in natural frequency (Liang, et al.,
1991; Chinchalkar, 2001; Al-Waily, 2013; Yang, et
al., 2016; Zhao, et al., 2016) and damping (Panteliou,
et al., 2001; Kyriazoglou, et al., 2004; Huang, et al.,
2016; Cao, et al., 2017).
Damage identification research is needed on the
sandwich ships-structure to prevent severe structural
failure. Laboratory testing was conducted to get data
which could be used as reference before being applied
to larger ship structures.
In this research, vibration-based damage
identification was conducted on sandwich plate
which designed for the main deck of a coal barge ship
using Finite Element (FEM) and Experimental Modal
Analysis (EMA) methods. Natural frequency and
damping ratio were used as a damage identification
parameter to distinguish the dynamic characteristics
of the intact (no damage) and damaged core in
sandwich plate structure.
2 METHOD
This research discusses the damage identification of
sandwich plate that was designed for the main deck
of a coal barge ship. The sandwich plate had 6 mm
thick steel faceplates and 15 mm thick core which was
fabricated from epoxy and rice husk powder. The
thickness of the faceplates and the core were designed
for the main deck of a coal barge ship (Thomson,
1981).
Core with the composition of 10% rice husk
powder and 15% rice husk powder was chosen to be
developed into a sandwich plate. These compositions
were selected because these cores met the Lloyd
Register standard (Yudiono, et al., 2018).
The natural frequency of the r-mode was
computed based on the highest value of the amplitude
on the frequency around the mode, as in equation (1)
where
!
"
is the amplitude in the r-mode and
#
"
is the
natural frequency estimation in r-mode.
$
!
"
%&#'
$
()*
+%#
"
+ #
,-).
(1)
Damping ratio was estimated using equation (2).
The ω1 and ω2 values were determined by procedure
depicted in Figure 1.
/
0
is the frequency at point 1
corresponding to the amplitude of (
1 234
/
5
6
),
/
7
is
the frequency at point 2 and.
8
9
is the damping ratio.
8
9
+%
/
0
:%/
7
7/
9
(2)
Figure 1: Damping ratio estimation.
Damage identification was used by detecting the
natural frequency and damping ratio of intact and
damaged sandwich plate having core made from rice-
hush powder. The dynamic characteristics of the two
sandwiches ware used as a reference to determine the
existence of a damage in a similar sandwich type.
Natural frequencies of the sandwich plate were
obtained by using Finite Element Method (FEM) and
Experimental Modal Analysis (EMA) method.
Damping ratio was obtained by EMA results. The
natural frequency and damping ratio of intact
sandwich and damaged sandwich could be compared.
Sandwich specimens had dimensions of 240 mm
x 60 mm x 27 mm. Damage was introduced to the
sandwich plate core. It was similar to the damage that
occurred in flexure tests, that was a damage with a
length of 15 mm and a depth of 35 mm (Yudiono, et
al., 2018).
2.1 FEM Set-up
Sandwich plate with core made from 10% rice husk
(S10RH) and sandwich plate with core made from
Damage Identification of the Sandwich Plate Having Core from Rice Husk-Epoxy for Ship Deck Structure
113
15% rice husk (S15RH) were analyzed using FEM to
estimate the value of natural frequency. The vibration
analysis used the first mode. The boundary condition
was a fix condition on both ends of the sandwich
model. The meshing process has been conducted on
the intact sandwich model and the damaged sandwich
model. The size of the meshing was 0.005 m.
2.2 EMA Set-up
Finite element analysis results were validated using
experiment. The sandwich plate specimen was placed
on a clamp that was strongly attached to the fraise
machine. The clamp served to fasten both ends of the
specimen. Experimental set-up of the specimen test
can be seen in Figure 2.
Figure 2: Experimental set-up of sandwich plate specimen
in EMA.
Data retrieval of dynamic characteristics from
specimen of sandwich plate used the instrument
arrangement as shown in Figure 3. The accelerometer
type is piezoelectric. The most widely used
Accelerometer type is piezoelectric (He & Fu, 2001).
The hammer was used as a source of vibration
(impact input). The accelerometer was used to
capture the vibration response from the sandwich
plate.
Figure 3: Instrument set-up of EMA.
To get the appropriate vibration response, it was
necessary to determine the proper configurations of
the hammer and the accelerometer. The
configurations of the hammer and accelerometer can
be seen in Figure 4. The raw data from the instrument
has been converted from the time domain to the
frequency domain using the Fourier Transform.
Figure 4: Configurations of hammer and accelerometer on
sandwich plate.
3 RESULT AND DISCUSSION
3.1 FEM Results
FEM was conducted to get the natural frequency from
the intact sandwich model and damaged sandwich
model in S10RH and S15RH. The material properties
of sandwich plate for FEM input was reported in
(Yudiono, et al., 2018).
Figure 5 (a) shows the intact sandwich model,
while Figure 5 (b) shows the damaged sandwich
model. The boundary condition was a fix condition
on both ends of the sandwich model, as shown in
Figure 6.
(a)
(b)
Figure 5: (a) Intact sandwich model (b) damaged sandwich
model.
SENTA 2018 - The 3rd International Conference on Marine Technology
114
Figure 6: Boundary conditions of the model.
The vibration analysis used was the first mode. The
mode shape of the sandwich model is shown in Figure
7. The natural frequency of intact S10RH and S15RH
were 635.13 Hz and 589.71 Hz respectively while the
natural frequency of damaged S10RH and S15RH
were 640.26 Hz and 560.22 Hz respectively.
Figure 7: Mode shapes of vibration analysis.
3.2 EMA Results
The original vibration data from EMA was in time
domain. The data were converted to frequency
domain using Fourier Transform so the value of
natural frequency of each sandwich plate has been
obtained. Figure 8 and Figure 9 show the spectrum of
vibration response in frequency domain. Figure 8
shows the vibration response spectrum of intact
sandwich plate and Figure 9 shows the vibration
response spectrum of damaged sandwich plate.
(a)
(b)
Figure 8: Vibration response spectrum of intact sandwich
with core made from (a) 10% (b) 15% rice husk powder.
(a)
(b)
Figure 9: Vibration response spectrum of damaged
sandwich with core made from (a) 10% and (b) 15% rice
husk powder.
The peak of the curve was the value of natural
frequency. The natural frequency of intact S10RH
and S15RH were 625.5 Hz and 575 Hz respectively.
The natural frequency of damaged sandwiches
S10RH and S15RH ware 623 Hz and 544 Hz
respectively.
3.3 Damage Identification of Sandwich
Plate using FEM and EMA
Damage identification of the sandwich plate having
core from rice husk-epoxy was conducted by using
FEM and EMA by identifying the natural frequency
deviation and the damping ratio deviation. The results
of numerical studies needed to be validated using the
results of the experimental study. In this research, the
Damage Identification of the Sandwich Plate Having Core from Rice Husk-Epoxy for Ship Deck Structure
115
results of FEM needed to be validated using the
results from EMA.
Table 1: Difference in the sandwich plate’s natural
frequency obtained using FEM and EMA in intact
condition.
Intact
sandwich
Differenc
e
(%)
FEM
EMA
10%
635.13
625.5
1.54
15%
589.71
575
2.56
Table 2: Difference in the sandwich plate’s natural
frequency obtained using FEM and EMA in damaged
condition.
Damaged
sandwich
Natural Frequency (Hz)
Difference
(%)
FEM
EMA
10%
640.26
623
2.77
15%
560.22
544
2.98
Table 1 shows the difference between FEM and
EMA in intact sandwich plate. While Table 2 shows
the difference between FEM and EMA in damaged
rice husk sandwich plate. FEM models of intact
S10RH and S15RH have FEM-EMA difference of
1.54% and 2.56%, respectively. FEM models of
damaged S10RH and S15RH have FEM-EMA
difference of 2.77% and 2.98%, respectively. FEM
model of intact S10RH has the lowest FEM-EMA
difference in first mode analysis.
The increased composition of the rice husk causes
an increase in the FEM-EMA difference because the
composite becomes increasingly non-homogeneous.
Composite characteristics that are not homogeneous,
can be modelled using orthotropic models. In
addition, natural frequency of the model should be
analyzed using other mode shape analysis.
Table 3: Natural frequency deviation in sandwich plate with
core made from 10% rice husk using FEM and EMA for
intact and damage conditions.
Method
Natural Frequency (Hz)
Natural
frequency
deviation
(%)
intact
sandwich
Damaged
sandwich
FEM
635.13
640.26
0.81
EMA
625.5
623
0.39
Table 4: Natural frequency deviation in sandwich plate with
core made from 15% rice husk using FEM and EMA for
intact and damage conditions.
Method
Natural Frequency (Hz)
Natural
frequency
deviation
(%)
Intact
sandwich
Damaged
sandwich
FEM
589.71
560.22
5.00
EMA
575
544
5.39
Table 3 shows the natural frequency deviation in
sandwich plate with core made from 10% rice husk
and Table 4 shows the natural frequency deviation in
sandwich plate with core made from 15% rice husk
by using FEM and EMA. Natural frequency deviation
due to damage from the S10RH rice husk is 0.39% by
EMA and 0.81 by FEM. Natural frequency deviation
due to damage from the sandwich 15% rice husk is
5.39% by EMA and 5.00 by FEM.
The natural frequency deviation data can be used
as damage identification parameter for sandwich
plate with core made from 10% and 15% rice husk.
Although S10RH and S15RH have the same damage
size, the sandwiches have different natural frequency
deviations. The value of natural frequency deviations
applies specifically to a sandwich plate. Different
sandwich plate has different natural frequency
deviations.
Table 5: Damping ratio of the sandwich plates for in intact
and damaged conditions.
Type of sandwich and rice husk
contents
Damping
ratio (%)
Intact - (10% rice husk powder)
0.96
Damaged - (10% rice husk powder)
0.8
Intact - (15% rice husk powder)
0.96
Damaged - (15% rice husk powder)
0.83
Damping ratio could also be used as a damage
identification parameter. Based on Table 5, intact
sandwich has a damping ratio 0.96%. For the
composition of 10% rice husk, damage causes a
deviation in the sandwich damping ratio by 0.16%.
For the composition of 15% rice husk, damage causes
a deviation in the sandwich damping ratio by 0.13%.
The natural frequency and damping ratio
deviation could be used as the damage identification
parameters for sandwich plate with core made from
10% and 15% rice husk. Nevertheless, sensitivity
analysis is still needed by varying the size of the
damage.
SENTA 2018 - The 3rd International Conference on Marine Technology
116
4 CONCLUSIONS
Sandwich plate has advantages and potential
applications to replace conventional steel stiffened
plate on ships structure. To ensure the structure’s
health and prevent sudden structural failure, it is
important to develop a damage identification method
for sandwich ships structure. In this research,
laboratory testing on sandwich plate was conducted
before testing on larger ship structures could be
performed
The experiment results showed that damage
caused decrease in the natural frequency of sandwich
with core made from 10% and 15% rice husk powder
by 0.39% and 5.39% respectively. The damping ratio
was changed due to damage; there were 0.16% and
0.13% changes observed for sandwich having core
made form 10% and 15% rice husk powder
respectively. Therefore, natural frequency and
damping ratio can be used as damage identification
parameters.
Sensitivity analysis in the size of damage needs to
be performed. In addition, better FEM model is
needed so the model can simulate damage in the core
and response of sandwich plate due to damage. The
identification of the damage location will be the main
concern for the next step of our research.
ACKNOWLEDGMENTS
This research was funded by Directorate of Research
and Community Services, Ministry of Research,
Technology and Higher Education, Republic of
Indonesia through PUPTN research scheme. Abdi
Ismail, the first author, gratefully thanks for the
support given by the Ministry through The Master’s
Degree Program Leading to Doctoral Degree for
Excellent Bachelor Graduates (PMDSU) fund.
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