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International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 10 Issue: 11 | Nov 2023 www.irjet.net p-ISSN: 2395-0072
© 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 603
Modal Analysis of Automotive Components
Pavan. H. K1, Shivashankar. R. Srivatsa2, G. Saravanakumar3
1P. G Student & Department of Mechanical Engineering, B M S C E Bangalore, 560019
2Assistant Professor & Department of Mechanical Engineering, B M S C E Bangalore, 560019
3 Associate Professor & Department of Mechanical Engineering, B M S C E Bangalore,
---------------------------------------------------------------------***---------------------------------------------------------------------
Abstract - This research paper explores the significance of
modal analysis in engineering for unveiling dynamic
characteristics like frequencies, mode shapes, and vibration
responses. It holds cross-disciplinary value, aiding aerospace,
civil, and mechanical engineering. The study employs both
experimental and software-based modal analysis techniques.
Experimental data is gathered through impact hammer and
accelerometers, validating software analysis outcomes. The
Finite Element Method is used for virtual structure creation,
refining it iteratively based on alignment with experimental
results. This methodology bridges the gap between physical
and virtual models, enhancing accuracy. The validation
process involves testing a plate with a hole under different
conditions, followed by experiments on a Rim in Free-Free
condition. Despite minor mode shape deviations, frequency
matches are close in all conditions, affirming analysis
reliability and its bridging role. The paper underscores the
interdisciplinary nature of modal analysis, contributing to
comprehensive engineering insights across various
applications.
Key Words: Mode Shapes, Altair Hyper Mesh,
Experimental, Validation.
Nomenclature: EMA: Experimental Modal Analysis. SMA:
software Modal Analysis.
1.INTRODUCTION
Modal analysis is an elementary techniqueusedinstructural
and mechanical engineering which is essential to
comprehend the dynamic behavior of the system. Itinvolves
identifying and examining the natural vibration modes,
which are found in structures and mechanical components.
These methods provide a detailed explanation of how a
system deforms and moves in response to external forces or
stimuli. Modal analysis is vital to recognize and solving
vibration-related problems as well as providing insight into
how structures react to different loading scenarios. It is
essential for the reliable functioning of complex systems in
the mechanical engineering, automobile design, industrial
machinery, and aerospace industries.
Empirical modal analysis is an essential aspect of
engineering and scientific research, dedicated to extracting
dynamic properties which captures natural vibrationmodes
and dynamic characteristics. EMA subjects’ structures to
controlled forces or stimuli, recordingsensordata tocapture
system responses.Througha rigorousmathematical method,
these data provide critical information on natural
frequencies, mode shapes, and damping ratios. The
importance of EMA extends to model validation, structural
integrity assessments, fault identification and system
performance improvements, with applications in civil
engineering,automotivedesignandmachinerymaintenance.
In addition, software model analysis predicts and analyzes
dynamic behaviors in mechanical systems and structures,
which makes it an effective computational tool in structural
analysis and engineering. In particular, it employs specific
software to replicate and analyze natural frequencies, mode
shapes, and damping ratios, thus prevents physical testing.
Software model analysis helps engineers and researchers in
assessing the system performance, improvised designs, and
solving issues in fields such as aerospace, civil engineering,
and automotive, accelerating the development much safer
and more efficient systems.
In basically, empirical model analysis integrates computer
models with experimental measurements to confirm the
accuracy of the models, hence verifying model analysis
software. This validation verifies the software's ability to
forecast natural frequencies, mode shapes, and damping
ratios with precision and servesasanacceptednorm.Design
optimization, structural health monitoring, and failure
prediction represent a few of its effects. These help
researchers and engineers make better decisions, enhance
system performance, and produce better work, all of which
advance the field of analysis of models and their various
industrial applications.
1.1 Methodology
During our validation stage, we investigated three different
scenarios: Fix-Free, Fix-Free, and Fix-Fix. A combination of
computer models and experimental techniques were
employed to carefully examine these situations. To ensure
that our chosen approaches were accurate and
trustworthy, at first, we analyzed frequencies and mode
shapes. Afterwards we narrowed down our research to the
Rim and focused on looking at the Free-Free condition. This
comprehensive method not only confirmed the validity of
our results but also made sure a significant addition to the
abundance of knowledge already available aboutthesystem
that was studied.
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 10 Issue: 11 | Nov 2023 www.irjet.net p-ISSN: 2395-0072
© 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 604
1.2 Plate Test Validation.
1.2.1 Experimental test setup: In this instance, in addition
to the standard testing proceduresand equipment whichare
explained below, we also test the object using the Impact
Hammer method.
a) Data Acquisition system: DEWE43V
b) Accelerometer: DYNAMIX SN 18226
c) Impact hammer: PCB SN 22826
d) Software: Dewesoft
To obtain a response from the system in this testingmethod,
we employed the rowing hammer approach. At first, we
calculated it for 48 nodes, with node 1 serving as the
response node. Then took 4 responses from each of the
nodes to average the relevant frequencies.
The Steel Plate is 410 mm long, 210 mm broad, and has a
50 mm diameter hole. It's made of material with a density of
7.9e-9 and a Young's modulus of 200 GPa. This material is
2.3 mm thick with a Poisson's ratio of 0.3. These
requirements, which are critical in engineeringandmaterial
science, control the mechanical properties of the object and
its’ usability for various applications such as structural
integrity tests or stress-strain investigations. The data
supplied here is used to evaluate its performance and
behaviour under various loads or situations.
Fig 1: Plate setup for Free-Free test condition
Fig 2: plate setup for Fix-Free test condition
Fig 3: Plate setup for Fix-Fix test condition
Fig 4: line geometry of plate for EMA
Figure 1 above shows a configuration for a Free-Free
modal analysis of a plate, with a plate and sponge arranged
on top of each other. Figure 2 showsa Fix-Freeconditionand
was composed of a plate and a long solid metal bar with four
C-clamps for fixing. Figure 3 shows the Fix-Fix condition,
which consists of 8 C-clamps and 2 long solid bars. Figure 4
shows the line geometry of the plate, which was generated
using Dewesoft software, and contains 48 nodes that may
receive responses from the plate.
3. 1.2.2 Software simulation test setup.
The Plate's geometry was created using Solid Works, Hyper
mesh was used to mesh for simulation purposes with Opti-
struct as solver.
Fig. 5: CAD model of Plate
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 10 Issue: 11 | Nov 2023 www.irjet.net p-ISSN: 2395-0072
© 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 605
Fig. 6: Finate Element Model of Plate
The Opti Struct solver was used to perform a 2D modal
analysis on a steel plate. The plate has a quad element count
of 1300 and an aspect ratio of 4.3. The mesh elements had a
maximum degree of skewness of 34 and a Jacobian value of
1, indicating that the mesh was well-structured. Modal
analysis is required for the study of a structure's natural
frequencies and mode shapes. This example provides
engineers with insights into the structural behaviours and
likely resonance frequencies of this steel plate, which is
critical for applications that use steel plates in a variety of
industries'
2. Frequencies and Mode Shapes of Plate
Table -1: Fix-Free modal analysis frequency
Table -2: Fix-Fix modal analysis frequency
Table -3: Free-Free modal analysis frequency
2.1 Fix-Free mode shapes Validation
Fig. 5: Fix-Free plate mode 1 EMA
Fig. 6: Fix-Free plate mode 1 SMA
Fig. 7: Fix-Free plate mode 2 EMA
Fig. 8: Fix-Free plate mode 2 SMA
Fig. 9: Fix-Free plate mode 3 EMA
SL
NO
EMA Frequency
In Hz
SMA frequency
In Hz
%
Variation
1 7.8 8.6 9.3
2 30 32 6.25
3 47.6 54 11.85
4 101.2 112 0.78
SL
NO
EMA Frequency
In Hz
SMA Frequency
In Hz
%
Variation
1 58 60 3.33
2 90 88 2.22
3 152 159 4.4
4 195 200 2.5
SL
NO
EMA Frequency
In Hz
SMA Frequency
In Hz
%
Variation
1 47.6 46.90 1.47
2 66 57.52 12.84
3 122 133.84 8.84
4 178 186 4.30
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 10 Issue: 11 | Nov 2023 www.irjet.net p-ISSN: 2395-0072
© 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 606
Fig. 10: Fix-Free plate mode 3 SMA
Fig. 11: Fix-Free plate mode 4 EMA
Fig. 12: Fix-Free plate mode 4 SMA
2.2 Fix-Fix mode shapes Validation Results
Fig. 13: Fix-Fix plate mode 1 EMA
Fig. 14: Fix-Fix plate mode 1 SMA
Fig. 15: Fix-Fix plate mode 2 EMA
Fig. 16: Fix-Fix plate mode 2 SMA
Fig. 17: Fix-Fix plate mode 3 EMA
Fig. 18: Fix-Fix plate mode 3 SMA
Fig. 19: Fix-Fix plate mode 4 EMA
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 10 Issue: 11 | Nov 2023 www.irjet.net p-ISSN: 2395-0072
© 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 607
Fig. 20: Fix-Fix plate mode 4 SMA
2.3 Free-Free mode shapes Validation Results
Fig. 21: Free-Free plate mode 1 EMA
Fig. 22: Free-Free plate mode 1 SMA
Fig. 23: Free-Free plate mode 2 EMA
Fig. 24: Free-Free plate mode 2 SMA
Fig. 25: Free-Free plate mode 3 EMA
Fig. 26 Free-Free plate mode 3 SMA
Fig. 27: Free-Free plate mode 4 EMA
Fig. 28: Free-Free plate mode 4 SMA
3. Rim Experimental Setup
Steel is used to make the rims, which have a Young's
modulus of 200 GPa, a density of 7.9e-9,anda Poisson'sratio
of 0.3. With a diameter of 330mm and a length of 112mm,
this steel rim is an essential component. These criteria are
critical for constructing and assessing cylindrical
components used in engineering and manufacturing
applications, such as rims for automobiles or equipment. An
evaluation of a material's mechanical properties is required
to assess its strength, deformation characteristics, and
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 10 Issue: 11 | Nov 2023 www.irjet.net p-ISSN: 2395-0072
© 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 608
overall performance under a variety of loads and
circumstances, as well as to ensure the dependability and
safety of the cylindrical structure it forms.
Fig. 29: Real Tested Steel Rim
Fig. 30: Free-Free Condition setup for Rim EMA
3.1 Rim Software Simulation Setup
The boundary condition and meshing part details will be
shown below. The geometry of the Rim was created using
Solid Works and Hyper mesh was utilized to mesh for
simulation purposes with Opti struct as solver.
Fig. 29: CAD model of Rim
Fig. 30: Finate Element Model of Rim
The Opti Struct solver was used to perform a 2D mid-mesh
free-free modal analysis with a massive quad mesh element
count of 230,456. The mesh's quality and readiness for
analysis were indicated by the aspect ratio of 4.1, maximum
skewness of 49 degrees, and Jacobian value of 0.91.
Understanding a structure's intrinsic vibrational modesand
frequencies is crucial for a variety of engineering
applications. This is possible because of free-free modal
analysis. It providesengineerswithinsightsintothedynamic
behaviour of the examined system in this scenario, allowing
them to analyse the system's susceptibility to external
pressures, resonance frequencies, and likely modes of
vibration, assisting in design optimisation and structural
integrity assessments.
3.2 Mode Shapes and Frequencies of the Rim
3.2.1 Frequency Table
Table.4: Free-Free modal analysis frequency
SL
NO
EMA Frequency
In Hz
SMA frequency
In Hz
%
Variation
1 311 302.33 2.89
2 782 821.792 4.75
3 1242 1264.74 1.7
4 1458 1371.81 H 5.96
3.2.2 Rim Mode Shapes
Fig. 31: Free-Free Rim mode 1 EMA
Fig. 32: Free-Free Rim mode 1 SMA
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 10 Issue: 11 | Nov 2023 www.irjet.net p-ISSN: 2395-0072
© 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 609
Fig. 33: Free-Free Rim mode 2 EMA
Fig. 34: Free-Free Rim mode 2 SMA
Fig. 35: Free-Free Rim mode 3 EMA
Fig. 36: Free-Free Rim mode 3 SMA
Fig. 37: Free-Free Rim mode 4 EMA
Fig. 38: Free-Free Rim mode 4 SMA
4. Conclusion
This research work has shown a striking convergence of
frequencies for the three different conditions: Free-Free,
Fixed-Free, and Fixed-Fixed. Even though slight differences
in mode forms were seen in the Free-Free state, these
differences are probably the outcome of the vacuum
circumstances and material ageing. This finding highlights
the resilience of the modal analysis techniques used in this
study and their constant applicability in a range of contexts.
The adaptability of modal analysis has been demonstrated
by this interdisciplinary approach, greatly advancing our
understanding of dynamic behaviors in a range of
applications. Through dependable modal analysis
approaches, this research has emphasized the confluence of
the virtual and physical realms, boosted our engineering
insights and fostered confidence in the precision of
predictive models.
This paper concludes by mentioning the importance
of modal analysis inunderstandingstructural behaviors. The
frequency matching, which stay consistent despite minor
variations, shows how reliable the approach is. These
findings improve our knowledge of dynamic reactionswhile
also supporting engineering practice. Thereby, this study
extends the field's techniques and expands our
understanding of dynamic processes, each of which
beneficial effects on a variety of real-world applications.
5. REFERENCES
[1] Akın Oktav, Experimental and numerical modal analysis
of a passenger vehicle, nternational Journal of Vehicle
Noise and Vibration · December 2016,
https://www.researchgate.net/publication/308625434
[2] Miroslav Mandal, “Modal analysis of cantilever beam”,
VSB Technical University of Ostrava;2013.
[3] F.Lembregts,Modalcorrelationforaxisymmetricmodels
with repeated roots – wheel rim case study, Siemens
Industry Software, Simulation & Test Solutions
Interleuvenlaan 68, B-3001, Leuven, Belgium e-mail:
frans.lembregts@siemens.com
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 10 Issue: 11 | Nov 2023 www.irjet.net p-ISSN: 2395-0072
© 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 610
[4] C. Lein, M. Beitelschmidt, Comparative study of model
correlation methods with application to model order
reduction,ISMA2014-USD2014ConferenceProceedings,
K.U. Leuven (2014), pp. 2683-2700.
[5] B. Peeters, H. Van der Auweraer, P. Guillaume, J.
Leuridan, The PolyMAX Frequency-Domain Method: A
New Standard for Modal Parameter Estimation? Shock
and Vibration, vol. 11, no. 3-4,
doi:10.1155/2004/523692 (2004), pp. 395-409
[6] Allemang, R.J.(1999)‘Analyticalandexperimentalmodal
analysis’, Lecture Notes, UCSDRL CN-20-263-662.
[7] Allemang, R.J. (2003) ‘The modal assurance criterion:
twenty years of use and abuse’, SoundandVibration,Vol.
37, No. 8, pp.14–23.
[8] Allemang, R.J. and Brown, D.L. (1982) ‘A correlation
coefficient formodal vector analysis’, Paperpresentedat
Proceedings of the 1st International Modal Analysis
Conference, SEM, Orlando.
[9] Chen, G. (2001) FE Model Validation for Structural
Dynamics, PhD thesis, University of London, UK.
[10] Chittilla, K., Yeola, Y., Tiwari, A. and Rajamanickam,
R. (2013) Effect of Excitation Methods on Experimental
Modal Analysis of Passenger Car Tire, SAE Technical
Paper 2013-01-2854.
[11] Davidsson, P. (2004) Structure-Acoustic Analysis:
Finite Element Modeling and Reduction Methods, PhD
thesis, Lund University, Lund, Sweden.
[12] Fuellekrug, U. (2008) ‘Computation of real normal
modes from complex eigenvectors’, Mechanical Systems
and Signal Processing, Vol. 22, No. 1, pp.57–65.
[13] Hanouf, Z.A. and Faris, W.F. (2009) ‘Investigation
into noise problems in vehicle structure using vibro-
acousticapproach’,InternationalJournalofVehicleNoise
and Vibration, Vol. 5, No. 3, pp.238–260.
[14] Hanouf, Z.A., Faris, W.F. and Noor, M.J.M. (2016)
‘Dynamic characterisation of vehicle structural panels’,
International Journal of Vehicle Noise andVibration,Vol.
11, Nos. 3–4, pp.199–209.
[15] Huston, R.L. and Liu, C.Q. (2011) Principles of
Vibration Analysis with Applications in Automotive
Engineering, pp.8–28, SAE International, Warrendale.
[16] Ibrahim, S.R. (1983) ‘Computation of normal modes
from identified complex modes’, AIAA Journal, Vol. 21,
No. 3, pp.446–451.
[17] Imamovic, N. (1998) Validation of Large Structural
Dynamics Models Using Modal Test Data, PhD thesis,
Imperial College, London, UK.

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Modal Analysis of Automotive Components

  • 1. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 10 Issue: 11 | Nov 2023 www.irjet.net p-ISSN: 2395-0072 © 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 603 Modal Analysis of Automotive Components Pavan. H. K1, Shivashankar. R. Srivatsa2, G. Saravanakumar3 1P. G Student & Department of Mechanical Engineering, B M S C E Bangalore, 560019 2Assistant Professor & Department of Mechanical Engineering, B M S C E Bangalore, 560019 3 Associate Professor & Department of Mechanical Engineering, B M S C E Bangalore, ---------------------------------------------------------------------***--------------------------------------------------------------------- Abstract - This research paper explores the significance of modal analysis in engineering for unveiling dynamic characteristics like frequencies, mode shapes, and vibration responses. It holds cross-disciplinary value, aiding aerospace, civil, and mechanical engineering. The study employs both experimental and software-based modal analysis techniques. Experimental data is gathered through impact hammer and accelerometers, validating software analysis outcomes. The Finite Element Method is used for virtual structure creation, refining it iteratively based on alignment with experimental results. This methodology bridges the gap between physical and virtual models, enhancing accuracy. The validation process involves testing a plate with a hole under different conditions, followed by experiments on a Rim in Free-Free condition. Despite minor mode shape deviations, frequency matches are close in all conditions, affirming analysis reliability and its bridging role. The paper underscores the interdisciplinary nature of modal analysis, contributing to comprehensive engineering insights across various applications. Key Words: Mode Shapes, Altair Hyper Mesh, Experimental, Validation. Nomenclature: EMA: Experimental Modal Analysis. SMA: software Modal Analysis. 1.INTRODUCTION Modal analysis is an elementary techniqueusedinstructural and mechanical engineering which is essential to comprehend the dynamic behavior of the system. Itinvolves identifying and examining the natural vibration modes, which are found in structures and mechanical components. These methods provide a detailed explanation of how a system deforms and moves in response to external forces or stimuli. Modal analysis is vital to recognize and solving vibration-related problems as well as providing insight into how structures react to different loading scenarios. It is essential for the reliable functioning of complex systems in the mechanical engineering, automobile design, industrial machinery, and aerospace industries. Empirical modal analysis is an essential aspect of engineering and scientific research, dedicated to extracting dynamic properties which captures natural vibrationmodes and dynamic characteristics. EMA subjects’ structures to controlled forces or stimuli, recordingsensordata tocapture system responses.Througha rigorousmathematical method, these data provide critical information on natural frequencies, mode shapes, and damping ratios. The importance of EMA extends to model validation, structural integrity assessments, fault identification and system performance improvements, with applications in civil engineering,automotivedesignandmachinerymaintenance. In addition, software model analysis predicts and analyzes dynamic behaviors in mechanical systems and structures, which makes it an effective computational tool in structural analysis and engineering. In particular, it employs specific software to replicate and analyze natural frequencies, mode shapes, and damping ratios, thus prevents physical testing. Software model analysis helps engineers and researchers in assessing the system performance, improvised designs, and solving issues in fields such as aerospace, civil engineering, and automotive, accelerating the development much safer and more efficient systems. In basically, empirical model analysis integrates computer models with experimental measurements to confirm the accuracy of the models, hence verifying model analysis software. This validation verifies the software's ability to forecast natural frequencies, mode shapes, and damping ratios with precision and servesasanacceptednorm.Design optimization, structural health monitoring, and failure prediction represent a few of its effects. These help researchers and engineers make better decisions, enhance system performance, and produce better work, all of which advance the field of analysis of models and their various industrial applications. 1.1 Methodology During our validation stage, we investigated three different scenarios: Fix-Free, Fix-Free, and Fix-Fix. A combination of computer models and experimental techniques were employed to carefully examine these situations. To ensure that our chosen approaches were accurate and trustworthy, at first, we analyzed frequencies and mode shapes. Afterwards we narrowed down our research to the Rim and focused on looking at the Free-Free condition. This comprehensive method not only confirmed the validity of our results but also made sure a significant addition to the abundance of knowledge already available aboutthesystem that was studied.
  • 2. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 10 Issue: 11 | Nov 2023 www.irjet.net p-ISSN: 2395-0072 © 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 604 1.2 Plate Test Validation. 1.2.1 Experimental test setup: In this instance, in addition to the standard testing proceduresand equipment whichare explained below, we also test the object using the Impact Hammer method. a) Data Acquisition system: DEWE43V b) Accelerometer: DYNAMIX SN 18226 c) Impact hammer: PCB SN 22826 d) Software: Dewesoft To obtain a response from the system in this testingmethod, we employed the rowing hammer approach. At first, we calculated it for 48 nodes, with node 1 serving as the response node. Then took 4 responses from each of the nodes to average the relevant frequencies. The Steel Plate is 410 mm long, 210 mm broad, and has a 50 mm diameter hole. It's made of material with a density of 7.9e-9 and a Young's modulus of 200 GPa. This material is 2.3 mm thick with a Poisson's ratio of 0.3. These requirements, which are critical in engineeringandmaterial science, control the mechanical properties of the object and its’ usability for various applications such as structural integrity tests or stress-strain investigations. The data supplied here is used to evaluate its performance and behaviour under various loads or situations. Fig 1: Plate setup for Free-Free test condition Fig 2: plate setup for Fix-Free test condition Fig 3: Plate setup for Fix-Fix test condition Fig 4: line geometry of plate for EMA Figure 1 above shows a configuration for a Free-Free modal analysis of a plate, with a plate and sponge arranged on top of each other. Figure 2 showsa Fix-Freeconditionand was composed of a plate and a long solid metal bar with four C-clamps for fixing. Figure 3 shows the Fix-Fix condition, which consists of 8 C-clamps and 2 long solid bars. Figure 4 shows the line geometry of the plate, which was generated using Dewesoft software, and contains 48 nodes that may receive responses from the plate. 3. 1.2.2 Software simulation test setup. The Plate's geometry was created using Solid Works, Hyper mesh was used to mesh for simulation purposes with Opti- struct as solver. Fig. 5: CAD model of Plate
  • 3. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 10 Issue: 11 | Nov 2023 www.irjet.net p-ISSN: 2395-0072 © 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 605 Fig. 6: Finate Element Model of Plate The Opti Struct solver was used to perform a 2D modal analysis on a steel plate. The plate has a quad element count of 1300 and an aspect ratio of 4.3. The mesh elements had a maximum degree of skewness of 34 and a Jacobian value of 1, indicating that the mesh was well-structured. Modal analysis is required for the study of a structure's natural frequencies and mode shapes. This example provides engineers with insights into the structural behaviours and likely resonance frequencies of this steel plate, which is critical for applications that use steel plates in a variety of industries' 2. Frequencies and Mode Shapes of Plate Table -1: Fix-Free modal analysis frequency Table -2: Fix-Fix modal analysis frequency Table -3: Free-Free modal analysis frequency 2.1 Fix-Free mode shapes Validation Fig. 5: Fix-Free plate mode 1 EMA Fig. 6: Fix-Free plate mode 1 SMA Fig. 7: Fix-Free plate mode 2 EMA Fig. 8: Fix-Free plate mode 2 SMA Fig. 9: Fix-Free plate mode 3 EMA SL NO EMA Frequency In Hz SMA frequency In Hz % Variation 1 7.8 8.6 9.3 2 30 32 6.25 3 47.6 54 11.85 4 101.2 112 0.78 SL NO EMA Frequency In Hz SMA Frequency In Hz % Variation 1 58 60 3.33 2 90 88 2.22 3 152 159 4.4 4 195 200 2.5 SL NO EMA Frequency In Hz SMA Frequency In Hz % Variation 1 47.6 46.90 1.47 2 66 57.52 12.84 3 122 133.84 8.84 4 178 186 4.30
  • 4. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 10 Issue: 11 | Nov 2023 www.irjet.net p-ISSN: 2395-0072 © 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 606 Fig. 10: Fix-Free plate mode 3 SMA Fig. 11: Fix-Free plate mode 4 EMA Fig. 12: Fix-Free plate mode 4 SMA 2.2 Fix-Fix mode shapes Validation Results Fig. 13: Fix-Fix plate mode 1 EMA Fig. 14: Fix-Fix plate mode 1 SMA Fig. 15: Fix-Fix plate mode 2 EMA Fig. 16: Fix-Fix plate mode 2 SMA Fig. 17: Fix-Fix plate mode 3 EMA Fig. 18: Fix-Fix plate mode 3 SMA Fig. 19: Fix-Fix plate mode 4 EMA
  • 5. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 10 Issue: 11 | Nov 2023 www.irjet.net p-ISSN: 2395-0072 © 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 607 Fig. 20: Fix-Fix plate mode 4 SMA 2.3 Free-Free mode shapes Validation Results Fig. 21: Free-Free plate mode 1 EMA Fig. 22: Free-Free plate mode 1 SMA Fig. 23: Free-Free plate mode 2 EMA Fig. 24: Free-Free plate mode 2 SMA Fig. 25: Free-Free plate mode 3 EMA Fig. 26 Free-Free plate mode 3 SMA Fig. 27: Free-Free plate mode 4 EMA Fig. 28: Free-Free plate mode 4 SMA 3. Rim Experimental Setup Steel is used to make the rims, which have a Young's modulus of 200 GPa, a density of 7.9e-9,anda Poisson'sratio of 0.3. With a diameter of 330mm and a length of 112mm, this steel rim is an essential component. These criteria are critical for constructing and assessing cylindrical components used in engineering and manufacturing applications, such as rims for automobiles or equipment. An evaluation of a material's mechanical properties is required to assess its strength, deformation characteristics, and
  • 6. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 10 Issue: 11 | Nov 2023 www.irjet.net p-ISSN: 2395-0072 © 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 608 overall performance under a variety of loads and circumstances, as well as to ensure the dependability and safety of the cylindrical structure it forms. Fig. 29: Real Tested Steel Rim Fig. 30: Free-Free Condition setup for Rim EMA 3.1 Rim Software Simulation Setup The boundary condition and meshing part details will be shown below. The geometry of the Rim was created using Solid Works and Hyper mesh was utilized to mesh for simulation purposes with Opti struct as solver. Fig. 29: CAD model of Rim Fig. 30: Finate Element Model of Rim The Opti Struct solver was used to perform a 2D mid-mesh free-free modal analysis with a massive quad mesh element count of 230,456. The mesh's quality and readiness for analysis were indicated by the aspect ratio of 4.1, maximum skewness of 49 degrees, and Jacobian value of 0.91. Understanding a structure's intrinsic vibrational modesand frequencies is crucial for a variety of engineering applications. This is possible because of free-free modal analysis. It providesengineerswithinsightsintothedynamic behaviour of the examined system in this scenario, allowing them to analyse the system's susceptibility to external pressures, resonance frequencies, and likely modes of vibration, assisting in design optimisation and structural integrity assessments. 3.2 Mode Shapes and Frequencies of the Rim 3.2.1 Frequency Table Table.4: Free-Free modal analysis frequency SL NO EMA Frequency In Hz SMA frequency In Hz % Variation 1 311 302.33 2.89 2 782 821.792 4.75 3 1242 1264.74 1.7 4 1458 1371.81 H 5.96 3.2.2 Rim Mode Shapes Fig. 31: Free-Free Rim mode 1 EMA Fig. 32: Free-Free Rim mode 1 SMA
  • 7. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 10 Issue: 11 | Nov 2023 www.irjet.net p-ISSN: 2395-0072 © 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 609 Fig. 33: Free-Free Rim mode 2 EMA Fig. 34: Free-Free Rim mode 2 SMA Fig. 35: Free-Free Rim mode 3 EMA Fig. 36: Free-Free Rim mode 3 SMA Fig. 37: Free-Free Rim mode 4 EMA Fig. 38: Free-Free Rim mode 4 SMA 4. Conclusion This research work has shown a striking convergence of frequencies for the three different conditions: Free-Free, Fixed-Free, and Fixed-Fixed. Even though slight differences in mode forms were seen in the Free-Free state, these differences are probably the outcome of the vacuum circumstances and material ageing. This finding highlights the resilience of the modal analysis techniques used in this study and their constant applicability in a range of contexts. The adaptability of modal analysis has been demonstrated by this interdisciplinary approach, greatly advancing our understanding of dynamic behaviors in a range of applications. Through dependable modal analysis approaches, this research has emphasized the confluence of the virtual and physical realms, boosted our engineering insights and fostered confidence in the precision of predictive models. This paper concludes by mentioning the importance of modal analysis inunderstandingstructural behaviors. The frequency matching, which stay consistent despite minor variations, shows how reliable the approach is. These findings improve our knowledge of dynamic reactionswhile also supporting engineering practice. Thereby, this study extends the field's techniques and expands our understanding of dynamic processes, each of which beneficial effects on a variety of real-world applications. 5. REFERENCES [1] Akın Oktav, Experimental and numerical modal analysis of a passenger vehicle, nternational Journal of Vehicle Noise and Vibration · December 2016, https://www.researchgate.net/publication/308625434 [2] Miroslav Mandal, “Modal analysis of cantilever beam”, VSB Technical University of Ostrava;2013. [3] F.Lembregts,Modalcorrelationforaxisymmetricmodels with repeated roots – wheel rim case study, Siemens Industry Software, Simulation & Test Solutions Interleuvenlaan 68, B-3001, Leuven, Belgium e-mail: frans.lembregts@siemens.com
  • 8. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 10 Issue: 11 | Nov 2023 www.irjet.net p-ISSN: 2395-0072 © 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 610 [4] C. Lein, M. Beitelschmidt, Comparative study of model correlation methods with application to model order reduction,ISMA2014-USD2014ConferenceProceedings, K.U. Leuven (2014), pp. 2683-2700. [5] B. Peeters, H. Van der Auweraer, P. Guillaume, J. Leuridan, The PolyMAX Frequency-Domain Method: A New Standard for Modal Parameter Estimation? Shock and Vibration, vol. 11, no. 3-4, doi:10.1155/2004/523692 (2004), pp. 395-409 [6] Allemang, R.J.(1999)‘Analyticalandexperimentalmodal analysis’, Lecture Notes, UCSDRL CN-20-263-662. [7] Allemang, R.J. (2003) ‘The modal assurance criterion: twenty years of use and abuse’, SoundandVibration,Vol. 37, No. 8, pp.14–23. [8] Allemang, R.J. and Brown, D.L. (1982) ‘A correlation coefficient formodal vector analysis’, Paperpresentedat Proceedings of the 1st International Modal Analysis Conference, SEM, Orlando. [9] Chen, G. (2001) FE Model Validation for Structural Dynamics, PhD thesis, University of London, UK. [10] Chittilla, K., Yeola, Y., Tiwari, A. and Rajamanickam, R. (2013) Effect of Excitation Methods on Experimental Modal Analysis of Passenger Car Tire, SAE Technical Paper 2013-01-2854. [11] Davidsson, P. (2004) Structure-Acoustic Analysis: Finite Element Modeling and Reduction Methods, PhD thesis, Lund University, Lund, Sweden. [12] Fuellekrug, U. (2008) ‘Computation of real normal modes from complex eigenvectors’, Mechanical Systems and Signal Processing, Vol. 22, No. 1, pp.57–65. [13] Hanouf, Z.A. and Faris, W.F. (2009) ‘Investigation into noise problems in vehicle structure using vibro- acousticapproach’,InternationalJournalofVehicleNoise and Vibration, Vol. 5, No. 3, pp.238–260. [14] Hanouf, Z.A., Faris, W.F. and Noor, M.J.M. (2016) ‘Dynamic characterisation of vehicle structural panels’, International Journal of Vehicle Noise andVibration,Vol. 11, Nos. 3–4, pp.199–209. [15] Huston, R.L. and Liu, C.Q. (2011) Principles of Vibration Analysis with Applications in Automotive Engineering, pp.8–28, SAE International, Warrendale. [16] Ibrahim, S.R. (1983) ‘Computation of normal modes from identified complex modes’, AIAA Journal, Vol. 21, No. 3, pp.446–451. [17] Imamovic, N. (1998) Validation of Large Structural Dynamics Models Using Modal Test Data, PhD thesis, Imperial College, London, UK.