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International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 09 | Sep 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 692
Harmonic Analysis of Cantilever Beam with and without Cracks
Sushmitha N1, Dr Manjunath N Hegde2
1MTECH Scholar, Structural Engineering, Dr. Ambedkar Institute of Technology, Bengaluru, Karnataka, India
2Professor-Dept.of Civil Engineering, Dr. Ambedkar Institute of Technology, Bengaluru, Karnataka, India
---------------------------------------------------------------------***----------------------------------------------------------------------
Abstract - Crack is one of the serious breakdowns that
decrease the serviceable life and lead to collapse of the
structures and structural element. Today, failure of structural
element and structures mostly takes place due to component
debility. Cracks present on the surface of the structural
element like beam, accounts changes in stiffness, significantly
depending upon the cracks depth and location. Unique
features of vibration can be utilized to perceive crack in
beams. The presence of cracks which impact the
demonstration of structures as well as the vibration
parameters like modal natural frequencies, mode shapes. By
modal analysis the vibration parameters such as Eigen
frequencies and mode shapes are obtained. In the present
work, harmonic analysis of cantilever steelandconcretebeam
cracked, un-cracked and multiple cracks at different depths
and locations are analyzed using SAP 2000 software, the
repercussion of crack parameters (crack position and crack
depth) on the vibration parameters of a cracked cantilever
beam are inspected by unique systems using finite element
analysis (FEA), using SAP2000 software.
Key Words: Crack deepness, Natural Frequency, Mode
Shape, Harmonic analysis, SAP, Cantilever beam etc...
1. INTRODUCTION
Every structure and its structural elements
experiences cracks or damages during its entire life span.
Cracks or damages occur either on the surface or inside the
structural element. Cracks are visibly repulsive and
bothersome for inhabitants, and if the cracks are neglected
they can impact the rectitude, security, durability and
firmness of the building. Cracks present on the surfaceofthe
structural element like beam, accounts changes in stiffness,
significantly depending upon the cracks depth and location.
These changes, results in a consequential effect on vibration
performance of a whole structure. To make sure the secure
performance of the structures, it is very essential to know
whether their structural elements are ridofcracks,andeven
if crack is present evaluate their boundary. The approaches
largely used for identification of cracks are direct processes
such as ultrasound, X-rays, etc. Anyhow, these approaches
have confirmed to be inactive and inappropriate in
inevitable circumstances, because they need costly and in-
detailed investigations. In-order to overcome these kinds of
inconveniences, in recent years, investigators has
concentrated on higher qualified methods in detecting
cracks that is using ‘vibration installed damage discover
method’.
The vibration based technique acts on this
determined influence of mode shapes and frequency. The
mode shapes and natural frequencies can be determined
either by experimentation or analysisthatitwouldbeableto
know the global actions of the assembly. The application of
vibration based technique has been discovered by a lot of
investigators above different procedures because they are
non-destructive, economical, quick and for the discovery of
one or more cracks in varying constructions and also for
detecting the cracks that exists inside the structure which
are not visible to naked eye. This method also evaluating the
durability of the structures by utilizing assessment of the
constructional natural frequencies is explained. It has been
displayed in what way evaluations made at one point in the
building can be implemented to identify, locate and
determine the damage. The system given utilizes finite-
element analysis (FEA), because this technique will be
allowed to use on any construction.
1.1 Objectives
The main objectives of the present study are as follows:
 To construct the cantilever steel and concretebeam
models with appropriate dimensions and to know
its response using SAP2000 software.
 To observe the behaviour of fissured, without
fissure and multiple fissured beam.
 Harmonic analysis is performed to obtain and to
study the response which includes Eigen
frequencies, Eigen vectors and displacement of
wholesome and fissured beam, for one-of-a-kind
fissure places and distance downwards and for
multiple fissures of each Cantilever steel and
concrete beam.
 And evaluation made between the variationsoffirst
three modes of herbal frequencies with fissure
intensity whilst fissure area changes.
1.2 Methodology
In this paper discussion made on simple harmonic
analysis of a healthy Cantilever steel and concrete beam and
a beam with cracks at different locations and depths and for
multiple cracks using SAP2000 software. Analysis is carried
out for the models are as follows;
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 09 | Sep 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 693
MODEL 1: Cantilever steel beam of box section is modeled
without and with cracks at different depths (10, 20, 30 mm)
and locations (0.5, 1.5, 2.5 m) and multiple cracks.
MODEL 2: Cantilever concrete beamis modeled without and
with cracks at different locations (0.2m, 0.5m, 0.8m) and
distance downwards (10, 20, 30mm)and multiple cracks.
Table-1: Properties of the beam
Steel Beam
Length of the beam 3 m
Width of the beam 0.092 m
Height of the beam 0.172 m
Thickness of the beam 0.0054 m
Modulus of elasticity 210 Gpa
Poisons ratio 0.3
Density 7850 kg/m3
Concrete Beam
Length of the beam 1 m
Width of the beam 0.05 m
Depth of the beam 0.1 m
Modulus of elasticity 22.36*106 kN/m2
Poisons ratio 0.2
Density 25kN/m3
2. Modal Analysis
The essential accessory in shudder evaluation is modal
evaluation. To figure out Eigen frequenciesandEigenvectors
of systems and its structural element is the main purpose of
the modal evaluation. Eigen frequencies and Eigen vectorsof
both fissured and without fissure beams through the use of
SAP software program has been obtained.
For harmonic analysis following steps considered are as
follows:
 Developing the model (cantilever beam) and
defining material propertiesand section properties.
 Meshing and assigning the boundary condition.
 Harmonic aid is utilized to measure outcome for
displacement, natural frequency.
 Set harmonic analysis and analyze the model.
 Evaluate the outcome in the fashion of pictorial
representation.
2.1 Equation of motion
- For Damped system.............. (1)
- For Un-damped system............. (2)
= 0 – Free vibration...................................... (3)
Harmonic Analysis
If load is harmonic the response is also harmonic
....................................................................... (4)
Where,
ω – Excitation frequency
t – Time period; K – Stiffness matrix; M – Mass matrix;
C = αM +βK – Damping matrix
Excitation Force
Corresponding response is expressed as
......................................................................... (5)
................................................ (6)
................................................... (7)
Substituting equations (5), (6), (7) in (1)
For )
The progressed strength and weight matrix due to
destructions are demonstrated as
Where,
Alternate in strength due to harm
Alternate weight due to harm
Unique strength matrix of size n x n
Unique regular weight matrix of size n x n
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 09 | Sep 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 694
As a result damping matrix can be acquired as
Fig -1: 2D view of Cantilever Healthy Steel Beam
Fig -2: 2D view of Cantilever Healthy Concrete Beam
3. Results and Discussion
In this part cantilever steel and concrete beam models with,
without cracks and multiple cracks are developed as shown
in fig- 1 and 2. Eigen frequencies, Eigen vectors and
displacement of fissured and without fissured beams are
obtained by performing modal analysis using SAP2000
software. The crack locations considered for the beam
models as 0.5, 1.5, 2.5m for steel and 0.2, 0.5, 0.8m for
concrete, for these crack locations crack deepness
considered are 10, 20, 30mm.
The comparison for displacement v/s frequency of healthy
and cracked beams at different locations graphs has been
plotted below.
Chart -1: The comparison graph of Frequency v/s
Displacement of Healthy steel beam and beam with crack
at different locations (0.5, 1.5, 2.5m)
Chart -2: The comparison graph of Frequency v/s
Displacement of Healthy concrete beam and beam with
crack at unlike locations (0.2, 0.5, 0.8m).
3.1 Eigen frequency of the fissured beam has been reduced
compared to a beam without fissureandtheEigenfrequency
of the beam with fissure near to the fixed support(0.5m)has
been in large part decreased in comparison to a beams with
fissure away from the support (1.5m, 2.5m)asshownbelow.
Chart -3: Comparative graph for Variation of Natural
Frequency of un-cracked and cracked steel beam at non-
identical crack locations
3.2 Eigen frequency of the fissured beam has been reduced
compared to a beam without fissure and Eigen frequency of
beam with fissure near to the fixed support (0.2m) has been
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 09 | Sep 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 695
in large part decreased in comparison to a beams with
fissure away from the support (0.5m, 0.8m).
Chart -4: Comparative graph for Variation of Natural
Frequency of un-cracked and cracked concrete beam at
non-identical crack locations.
4. Conclusions
Based on the results obtained the variations of Eigen
frequency and Eigen vectors because of presenceofcrack on
cantilever beam structural element, following conclusions
are done:
 Variations in Eigen frequencies and Eigen vectors
are because of variation in crack specifications
along with crack vicinity and crack deepness.
 Crack existing near to the fixed end support of the
cantilever beam decreasestheEigenfrequencythan
compared to crack existing away from the fixed
support. In this study from chart 3 - 4 we can
observe that reduction in natural frequencyismore
at crack location 0.2m for concrete and 0.5m for
steel compared to 0.5m, 0.8m(concrete)and 1.5m,
2.5m(steel).
 Displacement will be more for cracked beam
compared to healthy beam because of reduction in
stiffness.
In the present study from chart 1 and 2 we can
observe crack (0.5m steel and 0.2m concrete)
located near to the fixed end support has high
displacement than crack located away from the
fixed support ( 1.5m, 2.5m steel and 0.5m, 0.8m
concrete) and healthy beam.
4.1 Scope of future work:
 Different shapes of beams (I-Beam, round, pipe).
 Structures like communication towers, turbine
shafts and structural elements like simply
supported beam, fixed beam with point load can be
analyzed.
 Damage identification in structures and structural
elements for different forms of materials.
 Different forms of cracks and viewpoint.
REFERENCES
[1] Elshamy M. and Crosby W.A, Elhadary M. “Crack
detection of cantilever beam by natural frequency
tracking using experimental andfinite elementanalysis”
Alexandria Engineering Journal 57, 3755-3766, 23
October 2018.
[2] Kaushar H. Barad, and SharmaD. S, Vishal Vyas “Crack
detection in cantilever beam by frequency based
method” Procedia Engineering volume 51, 770 – 775,
2013.
[3] Mehta P, Kureshi A, Patel N and Sharma D “Detection of
Cracks in a Cantilever Beam Using Signal Processingand
Strain Energy Based Model” IOP Conf. Series: Materials
Science and Engineering 234 012008, 2017.
[4] Amit Banerjee, and Pohit G “Crack Investigation of
Rotating Cantilever Beam by Fractal Dimension
Analysis” Procedia Technology 14, 188 – 195, 2014.
[5] Murat Kisa “Free vibration analysis of a cantilever
composite beam with multiple cracks”
www.elsevier.com/locate/compscitech Composites
Science and Technology volume 64, 1391–1402, 2003.
[6] Liew K. M. and Wang Q “Application Of Wavelet theory
for Crack Identification in Structures” J. Eng. Mech.
1998.124:152-157,from ascelibrary.orgonJan7th 2013.
[7] Zhang Xiaoqing, Han Qiang, and Li Feng “Analytical
Approach for Detection of Multiple Cracks in a
Beam”DOI:10.1061(ASCE)0733-9399,136:3(345),from
ascelibrary.org on June 6th 2013.
[8] Viola E, Nobile L and L. Federacy “Formulation of
Cracked Beam Element for Structural Analysis” DOI:
10.1061(ASCE) 0733-9399, 128:2(220), from
ascelibrary.org on June 10th 2013.

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  • 1. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 09 | Sep 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 692 Harmonic Analysis of Cantilever Beam with and without Cracks Sushmitha N1, Dr Manjunath N Hegde2 1MTECH Scholar, Structural Engineering, Dr. Ambedkar Institute of Technology, Bengaluru, Karnataka, India 2Professor-Dept.of Civil Engineering, Dr. Ambedkar Institute of Technology, Bengaluru, Karnataka, India ---------------------------------------------------------------------***---------------------------------------------------------------------- Abstract - Crack is one of the serious breakdowns that decrease the serviceable life and lead to collapse of the structures and structural element. Today, failure of structural element and structures mostly takes place due to component debility. Cracks present on the surface of the structural element like beam, accounts changes in stiffness, significantly depending upon the cracks depth and location. Unique features of vibration can be utilized to perceive crack in beams. The presence of cracks which impact the demonstration of structures as well as the vibration parameters like modal natural frequencies, mode shapes. By modal analysis the vibration parameters such as Eigen frequencies and mode shapes are obtained. In the present work, harmonic analysis of cantilever steelandconcretebeam cracked, un-cracked and multiple cracks at different depths and locations are analyzed using SAP 2000 software, the repercussion of crack parameters (crack position and crack depth) on the vibration parameters of a cracked cantilever beam are inspected by unique systems using finite element analysis (FEA), using SAP2000 software. Key Words: Crack deepness, Natural Frequency, Mode Shape, Harmonic analysis, SAP, Cantilever beam etc... 1. INTRODUCTION Every structure and its structural elements experiences cracks or damages during its entire life span. Cracks or damages occur either on the surface or inside the structural element. Cracks are visibly repulsive and bothersome for inhabitants, and if the cracks are neglected they can impact the rectitude, security, durability and firmness of the building. Cracks present on the surfaceofthe structural element like beam, accounts changes in stiffness, significantly depending upon the cracks depth and location. These changes, results in a consequential effect on vibration performance of a whole structure. To make sure the secure performance of the structures, it is very essential to know whether their structural elements are ridofcracks,andeven if crack is present evaluate their boundary. The approaches largely used for identification of cracks are direct processes such as ultrasound, X-rays, etc. Anyhow, these approaches have confirmed to be inactive and inappropriate in inevitable circumstances, because they need costly and in- detailed investigations. In-order to overcome these kinds of inconveniences, in recent years, investigators has concentrated on higher qualified methods in detecting cracks that is using ‘vibration installed damage discover method’. The vibration based technique acts on this determined influence of mode shapes and frequency. The mode shapes and natural frequencies can be determined either by experimentation or analysisthatitwouldbeableto know the global actions of the assembly. The application of vibration based technique has been discovered by a lot of investigators above different procedures because they are non-destructive, economical, quick and for the discovery of one or more cracks in varying constructions and also for detecting the cracks that exists inside the structure which are not visible to naked eye. This method also evaluating the durability of the structures by utilizing assessment of the constructional natural frequencies is explained. It has been displayed in what way evaluations made at one point in the building can be implemented to identify, locate and determine the damage. The system given utilizes finite- element analysis (FEA), because this technique will be allowed to use on any construction. 1.1 Objectives The main objectives of the present study are as follows:  To construct the cantilever steel and concretebeam models with appropriate dimensions and to know its response using SAP2000 software.  To observe the behaviour of fissured, without fissure and multiple fissured beam.  Harmonic analysis is performed to obtain and to study the response which includes Eigen frequencies, Eigen vectors and displacement of wholesome and fissured beam, for one-of-a-kind fissure places and distance downwards and for multiple fissures of each Cantilever steel and concrete beam.  And evaluation made between the variationsoffirst three modes of herbal frequencies with fissure intensity whilst fissure area changes. 1.2 Methodology In this paper discussion made on simple harmonic analysis of a healthy Cantilever steel and concrete beam and a beam with cracks at different locations and depths and for multiple cracks using SAP2000 software. Analysis is carried out for the models are as follows;
  • 2. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 09 | Sep 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 693 MODEL 1: Cantilever steel beam of box section is modeled without and with cracks at different depths (10, 20, 30 mm) and locations (0.5, 1.5, 2.5 m) and multiple cracks. MODEL 2: Cantilever concrete beamis modeled without and with cracks at different locations (0.2m, 0.5m, 0.8m) and distance downwards (10, 20, 30mm)and multiple cracks. Table-1: Properties of the beam Steel Beam Length of the beam 3 m Width of the beam 0.092 m Height of the beam 0.172 m Thickness of the beam 0.0054 m Modulus of elasticity 210 Gpa Poisons ratio 0.3 Density 7850 kg/m3 Concrete Beam Length of the beam 1 m Width of the beam 0.05 m Depth of the beam 0.1 m Modulus of elasticity 22.36*106 kN/m2 Poisons ratio 0.2 Density 25kN/m3 2. Modal Analysis The essential accessory in shudder evaluation is modal evaluation. To figure out Eigen frequenciesandEigenvectors of systems and its structural element is the main purpose of the modal evaluation. Eigen frequencies and Eigen vectorsof both fissured and without fissure beams through the use of SAP software program has been obtained. For harmonic analysis following steps considered are as follows:  Developing the model (cantilever beam) and defining material propertiesand section properties.  Meshing and assigning the boundary condition.  Harmonic aid is utilized to measure outcome for displacement, natural frequency.  Set harmonic analysis and analyze the model.  Evaluate the outcome in the fashion of pictorial representation. 2.1 Equation of motion - For Damped system.............. (1) - For Un-damped system............. (2) = 0 – Free vibration...................................... (3) Harmonic Analysis If load is harmonic the response is also harmonic ....................................................................... (4) Where, ω – Excitation frequency t – Time period; K – Stiffness matrix; M – Mass matrix; C = αM +βK – Damping matrix Excitation Force Corresponding response is expressed as ......................................................................... (5) ................................................ (6) ................................................... (7) Substituting equations (5), (6), (7) in (1) For ) The progressed strength and weight matrix due to destructions are demonstrated as Where, Alternate in strength due to harm Alternate weight due to harm Unique strength matrix of size n x n Unique regular weight matrix of size n x n
  • 3. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 09 | Sep 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 694 As a result damping matrix can be acquired as Fig -1: 2D view of Cantilever Healthy Steel Beam Fig -2: 2D view of Cantilever Healthy Concrete Beam 3. Results and Discussion In this part cantilever steel and concrete beam models with, without cracks and multiple cracks are developed as shown in fig- 1 and 2. Eigen frequencies, Eigen vectors and displacement of fissured and without fissured beams are obtained by performing modal analysis using SAP2000 software. The crack locations considered for the beam models as 0.5, 1.5, 2.5m for steel and 0.2, 0.5, 0.8m for concrete, for these crack locations crack deepness considered are 10, 20, 30mm. The comparison for displacement v/s frequency of healthy and cracked beams at different locations graphs has been plotted below. Chart -1: The comparison graph of Frequency v/s Displacement of Healthy steel beam and beam with crack at different locations (0.5, 1.5, 2.5m) Chart -2: The comparison graph of Frequency v/s Displacement of Healthy concrete beam and beam with crack at unlike locations (0.2, 0.5, 0.8m). 3.1 Eigen frequency of the fissured beam has been reduced compared to a beam without fissureandtheEigenfrequency of the beam with fissure near to the fixed support(0.5m)has been in large part decreased in comparison to a beams with fissure away from the support (1.5m, 2.5m)asshownbelow. Chart -3: Comparative graph for Variation of Natural Frequency of un-cracked and cracked steel beam at non- identical crack locations 3.2 Eigen frequency of the fissured beam has been reduced compared to a beam without fissure and Eigen frequency of beam with fissure near to the fixed support (0.2m) has been
  • 4. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 09 | Sep 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 695 in large part decreased in comparison to a beams with fissure away from the support (0.5m, 0.8m). Chart -4: Comparative graph for Variation of Natural Frequency of un-cracked and cracked concrete beam at non-identical crack locations. 4. Conclusions Based on the results obtained the variations of Eigen frequency and Eigen vectors because of presenceofcrack on cantilever beam structural element, following conclusions are done:  Variations in Eigen frequencies and Eigen vectors are because of variation in crack specifications along with crack vicinity and crack deepness.  Crack existing near to the fixed end support of the cantilever beam decreasestheEigenfrequencythan compared to crack existing away from the fixed support. In this study from chart 3 - 4 we can observe that reduction in natural frequencyismore at crack location 0.2m for concrete and 0.5m for steel compared to 0.5m, 0.8m(concrete)and 1.5m, 2.5m(steel).  Displacement will be more for cracked beam compared to healthy beam because of reduction in stiffness. In the present study from chart 1 and 2 we can observe crack (0.5m steel and 0.2m concrete) located near to the fixed end support has high displacement than crack located away from the fixed support ( 1.5m, 2.5m steel and 0.5m, 0.8m concrete) and healthy beam. 4.1 Scope of future work:  Different shapes of beams (I-Beam, round, pipe).  Structures like communication towers, turbine shafts and structural elements like simply supported beam, fixed beam with point load can be analyzed.  Damage identification in structures and structural elements for different forms of materials.  Different forms of cracks and viewpoint. REFERENCES [1] Elshamy M. and Crosby W.A, Elhadary M. “Crack detection of cantilever beam by natural frequency tracking using experimental andfinite elementanalysis” Alexandria Engineering Journal 57, 3755-3766, 23 October 2018. [2] Kaushar H. Barad, and SharmaD. S, Vishal Vyas “Crack detection in cantilever beam by frequency based method” Procedia Engineering volume 51, 770 – 775, 2013. [3] Mehta P, Kureshi A, Patel N and Sharma D “Detection of Cracks in a Cantilever Beam Using Signal Processingand Strain Energy Based Model” IOP Conf. Series: Materials Science and Engineering 234 012008, 2017. [4] Amit Banerjee, and Pohit G “Crack Investigation of Rotating Cantilever Beam by Fractal Dimension Analysis” Procedia Technology 14, 188 – 195, 2014. [5] Murat Kisa “Free vibration analysis of a cantilever composite beam with multiple cracks” www.elsevier.com/locate/compscitech Composites Science and Technology volume 64, 1391–1402, 2003. [6] Liew K. M. and Wang Q “Application Of Wavelet theory for Crack Identification in Structures” J. Eng. Mech. 1998.124:152-157,from ascelibrary.orgonJan7th 2013. [7] Zhang Xiaoqing, Han Qiang, and Li Feng “Analytical Approach for Detection of Multiple Cracks in a Beam”DOI:10.1061(ASCE)0733-9399,136:3(345),from ascelibrary.org on June 6th 2013. [8] Viola E, Nobile L and L. Federacy “Formulation of Cracked Beam Element for Structural Analysis” DOI: 10.1061(ASCE) 0733-9399, 128:2(220), from ascelibrary.org on June 10th 2013.