Numerical study on complex shaped cracks in cantilever beams concerning frequency and stiffness changes
Cristian Tufisi^{1} , GilbertRainer Gillich^{2} , Dorian Nedelcu^{3} , CodrutaOana Hamat^{4}
^{1, 2, 3, 4}Universitatea “Eftimie Murgu” din Resita, Resita, Romania
^{1}Corresponding author
Vibroengineering PROCEDIA, Vol. 19, 2018, p. 253258.
https://doi.org/10.21595/vp.2018.20123
Received 23 July 2018; accepted 6 August 2018; published 24 September 2018
JVE Conferences
The paper presents a mathematical relation to express the effects of a Tshaped crack on beamlike structures. The study is performed by using the finite element method (FEM) and contrived analytical formulas for proving the existing correlation between deflection, strain energy, and natural frequency changes. The damaged beam static and dynamic behaviors are analyzed by means of the FEM. The frequency shift for the first mode of vibration derived directly was compared with the frequency alteration calculated involving the change in the beam deflection for several scenarios of the Tshaped crack. The frequency shift is derived using the relations between deflection and natural frequency. As the final step in the research, we compared the outcomes for the same crack with the results achieved from a beam suffering a loss of stiffness.
Keywords: natural frequency, stiffness, deflection, damage severity, Tshaped crack.
1. Introduction
Damages can modify both the physical properties of a structure (mass, stiffness) as well as its dynamic characteristics (natural frequencies, damping ratio, and modal shapes and curvature). The stiffness loss reduces the capacity of a structure to store energy, and it directly depends on the position [14], respectively on the shape and depth of the crack [58]. The theory was also developed for changing environment [911], variable beam crosssection [12] and multiple cracks [13, 14].
In previous studies [1518], the authors developed a robust method for detecting, locating and evaluating transverse cracks in all types of beams, regardless of the constraining method, based on the natural frequency changes.
This paper presents a numerical study destined to find the dynamic response of beams with Tshaped cracks, in particular, the effect of the depth and position of the transverse crack component, using both analytical and FEM simulation methods.
2. Materials and methods
The research focuses on finding the effect of a branched crack on the natural frequencies of beamlike structures. To this aim, a steel beam, fixed on the left end and free at the other one (i.e. a cantilever beam) is considered in the study. It has the following key dimensions: the length $L=$ 1000 mm, the width $B=$ 50 mm and the thickness $H=$ 5 mm. hence, the intact beam has a crosssectional area and the moment of inertia $I=$ 52083.33 mm^{4}.
Table 1. Physicalmechanical properties of the structural steel as defined in the ANSYS library
Mass density
[kg/m^{3}]

Young modulus
[N/m^{2}]

Poisson
ratio

Tensile strength
[MPa]

Yield strength
[MPa]

Min. elongation [%]

7850

2·10^{11}

0.3

470630

355

20

The relevant physicalmechanical properties, presented in Table 1, are extracted from the ANSYS library for a structural steel.
For the cantilever beam, the damage geometry is described as a Tshaped crack, resulted from a transverse component followed by a longitudinal branch, with its general dimensions presented in Fig. 1.
Fig. 1. The geometry of a branched crack of ,,T” shape
The transverse component extends from the upper surface of the beam to the longitudinal crack. We considered 5 different scenarios, by studying the effects of different depths ,,$a$” of the Tshaped crack, starting from the upper surface of the beam $a=$ 0.5 mm and further increasing it with a step of 0.5 mm until it reaches $a=$ 2.5 mm, as illustrated in Fig. 1.
2.1. The finite element model of the test structure
In order to obtain the natural frequency and deflection of the damaged cantilever beam, two types of studies have been carried out, having the boundary conditions for the fixed end at the left extremity of the analyzed beam imposed by applying the fixed support constraint. For the static analysis, we applied a gravitational acceleration of 9.806 m/s^{2}.
The intact beam was meshed by using hexahedral elements of maximum 2 mm size, resulting in a model containing 39501 elements and 197961 nodes. As illustrated in Fig. 2 for the crack depth 0.5, 1 and 1.5 mm, for the beam with Tshaped crack at the different depth, the resulted mesh is even finer because the elements are deformed in the interface between the intact beam and damage boundary.
Fig. 2. a) a zoom on the left beam end for the intact beam, b)d) the damaged beam, highlighting the prismatic element’s distribution
a)
b)
c)
d)
In addition, the defect location, for all damage cases was replaced by a segment of reduced thickness $h=Ha$, thus a smaller stiffness (see Fig. 3). To compensate for the loss of mass we increased the mass density of the segment to $\widehat{\rho}=$ 15700 kg/m^{3}.
Fig. 3. A zoom on the segment with a reduced thickness
2.2. The finite element model of the test structure
The static and dynamic characteristics of the cantilever beam where studied by means of finite element analysis with the ANSYS software, for all damage scenarios positioned at the distance $x=$ 35 mm and at $x=$ 500 mm from the fixed end, resulting in a number of 22 studies, including the undamaged beam analysis. Two types of simulations where performed, by using:
• Modal module for determining the natural frequencies for the cantilever beam for the first six weak axis bending modes.
• Static structural for determining the deflection of the beam at the free end.
In this study, we iteratively increase the depth of the crack’s transversal component by a step $s=$ 0.5 mm, starting from the upper surface of the cantilever and evolving to the beam center. The first location of the damage is at position $x=$ 35 mm, and further, we analyzed the effect of the damage placed at $x=$ 500 mm from the fixed end. The beam with the reduced crosssection, nominated herein as the beam with a gap, is also implied in this study. The deflection increase at the cantilever beam’s free end due to damage, for the beam statically loaded with its own mass, and the natural frequencies are acquired.
From paper [15], the beam’s free end deflection for the healthy ${\delta}_{U}$ and damaged ${\delta}_{D}$ state is expressed by the mathematical relations:
The natural frequencies for the undamaged cantilever beam are given in accordance to the EulerBernoulli theory [11] with the relation:
From Eq. (1) and (2) we obtain:
After substituting Eq. (4) and (5) in Eq. (3), one obtains:
The natural frequency of the damaged beam results, from Eq. (6) and Eq. (7), as:
where $k\left(a,l\right)$ is the correction coefficient.
In consequence, the relation of the normalized frequency shift can be found as:
which is, in fact, the damage severity derived for the crack located at the fixed end of the beam.
Knowing the deflection of the free end for both healthy and damaged beam, we calculated the correction coefficient and afterwards the frequency of the damaged beam in respect to the natural frequency of the intact beam, in accordance to Eq. (8). The results were compared with the frequencies of the damaged beam obtained directly from the FEM analysis, in order to prove that the correction coefficient $k\left(a,l\right)$ and the severity can be used also for Tshaped cracks.
3. Results and discussions
To determine the correlation between the dynamic response and the changes in the deflection of cantilever beams, which occur due to different damage depth and positions, we compared the frequency changes obtained through modal analysis and the results calculated with Eq. (8) supported by static analysis for a crack with an inverted Tshape. Afterwards, we compared, the Tshaped crack with the results achieved from a beam having a rectangular gap with the fundamental dimensions as following: depth $a=$ 0.5, ..., 2.5 mm increased iteratively by a step $s=$ 0.5 mm and the longitudinal extend $l=$ 30 mm, equal to that of the crack.
The correction coefficient $k\left(a,l\right)$ is calculated from the deflection at the free end of the cantilever beam derived by means of the FEM. The natural frequency changes for the first weakaxis vibration mode are compared to those obtained by employing the Hybrid method, hence by applying the correction coefficient in Eq. (8). The results, as well as the attained errors, are presented in Table 2.
Table 2. Comparison of frequencies obtained from FEM and calculated involving the Hybrid method
$x$
[mm]

$a$
[mm]

${\delta}_{U}$
[mm]

${\delta}_{D}$
[mm]

$\kappa \left(a,l\right)$
[]

${f}_{iU}$
[Hz]

${f}_{i{D}_{FEM}}$
[Hz]

${f}_{i{D}_{hybrid}}$
[Hz]

Error
[%]

35

0.5

22.948

23.864

0.9806

4.088

4.0101

4.0088

0.03

1

24.532

0.9671

3.8914

3.8913

0.00


1.5

24.031

0.9772

3.7155

3.7174

0.05


2

32.031

0.8464

3.4548

3.4602

0.16


2.5

40.295

0.7546

3.0747

3.0850

0.33


500

0.5

23.076

0.9972

4.0795

4.0766

0.07


1

23.281

0.9928

4.0628

4.0587

0.10


1.5

23.619

0.9856

4.0357

4.0295

0.15


2

24.215

0.9734

3.9889

3.9796

0.23


2.5

25.368

0.9511

3.8844

3.8881

0.10

Additionally, we compared the modal FEM analysis and calculated results of the different damage position with that of the gap study. The results are presented in Table 3. The diagram obtained employing both the FEM and the hybrid FEManalytical methods are presented in Fig. 4 for crack position at $x=$ 35 mm and for $x=$ 500 mm, respectively.
From Table 3 and from the Fig. 4 one can observe that comparing the frequencies obtained directly from FEM and calculated involving the hybrid FEManalytical method for a Tshaped crack positioned near the fixed end and afterwards at the center of the beam, the errors are less that 0.33 %. The extremely small errors proved the precision achieved by using the correction coefficient $k\left(a,l\right)$ and qualifies the method for prediction of frequency changes due to Tshaped cracks with known parameters.
Table 3. Comparison of frequencies obtained from FEM simulation and Hybrid method for the Tshaped crack and the beam with a gap
$x$
[mm]

$a$
[mm]

FEM

Hybrid


${f}_{{i}_{GAP}}$
[Hz]

${f}_{iD}$
[Hz]

Error
[%]

${f}_{{i}_{GAP}}$
[Hz]

${f}_{iD}$
[Hz]

Error
[%]


35

0.5

4.0086

4.0088

0.04

4.0072

4.009

0.04

1

3.889

3.8913

0.06

3.8888

3.891

0.06


1.5

3.7126

3.7174

0.08

3.7145

3.717

0.08


2

3.4517

3.4602

0.09

3.4570

3.460

0.09


2.5

3.0689

3.0850

0.19

3.0791

3.085

0.19


500

0.5

4.057

4.0766

0.55

4.0364

4.077

1.00

1

4.046

4.0587

0.42

4.0284

4.059

0.75


1.5

4.0244

4.0295

0.28

4.0093

4.030

0.50


2

3.983

3.9796

0.15

3.9691

3.980

0.26


2.5

3.9006

3.8881

0.42

3.8861

3.888

0.05

Fig. 4. Comparison of frequencies obtained by FEM modal analysis and involving the hybrid method at crack position a) $x=$ 35 mm and b) $x=$ 500 mm
a)
b)
Table 3 shows that the beam with a gap instead of the Tshaped crack can substitute the crack in modeling the dynamic behavior of damaged beams. The error noticed here is less than 0.2 %, if the crack is present near the fixed end of the beam. For the crack positioned at 500 mm from the fixed end the maximum error is 1 %, showing that even if the error is larger than the previous study, the method still qualifies as a reliable damage indicator.
4. Conclusions
This paper presents the correlation between deflection, strain energy and natural frequency changes for beamlike structures by involving original mathematical relations. The methods presented show that the beams diminished capacity to store energy due to a crack through simple static analysis is a precise damage severity indicator. It was also proved that this indicator can be used even if the damage is not located at the position where the bending moment achieves maxima. Following, the effect of damage location was analyzed and it was shown that, if the crack is not located in the slice where the bending moment achieves maxima, its effect on the natural frequency changes is diminished in concordance to the normalized square of the mode shape curvature of the damaged slice in the intact state.
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