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International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 06 | June 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 3358
DISTORTION IN EN-8 PLATES HAVING DIFFERENT THICKNESS AND
CROSS SECTIONS USING MANUAL ELECTRIC ARC WELDING
ABHAY KUMAR MISHRA1, VIKAS KUMAR SHUKLA2, RATI SALUJA3
1M.Tech research scholar, GITM, Lucknow, UP, India
2Assistant Professor Dept. of Mechanical Engineering, GITM, Lucknow, UP, India
3P.hd research scholar, Dept. of Mechanical Engineering, Integral University, Lucknow, UP, India
---------------------------------------------------------------------***----------------------------------------------------------------------
Abstract - Welding is a process of joining two or more
similar or dissimilar material with the application of heat
with or without the application of filler material and
pressure in which heat is supplied either electrically or by
means of a gas torch. Welding is an important process for
fabrication of engineering components.
It has vast applications in ship buildings, constructions,
aerospace, automobile industries, etc. There are different
welding defects due to which weldments fails under service
conditions and cause damage to the property and loss of
human lives. In this work we are going to study one of the
most important welding defects known as Distortion.
Distortion is the change in shape and variation between the
positions of the two plates before welding andafter welding.
Distortion occurs due to good amount of temperature
difference at different points along the joint and thus at any
instant certain area of base metal expands and other
including weld bead contract.
In this work we are going to study how much distortion
occur in medium carbon steel that is EN-8 Plates of various
cross-sections and thickness. This study is done by
experiment and justify the result using ANOVA.
Key Words: Distortion, Mild Steel, EN-8, Butt Joint, Arc
Welding & Single V Groove, ANOVA
1. INTRODUCTION OF DISTORTION
The term distortion means deviation from desired or actual
shape and size. In welding terminology distortionmeansthe
local residual deformation resulting from welding which
changes the dimension and shape of the work-piece joined.
While doing welding when the welding operator used eye
shield and electrode holder, commenced welding a job,
starting and finishing at any place. After completion of the
job if it was found distorted and it was taken forgrantedthat
it could not be avoided. The impression was all welding
caused distortion. That why think of it.
This was purely ignorance, because distortion can be
controlled and minimized by approaching the job holding in
the correct manner.
At present era, welding can be done with minimum
distortion. For example, different machines beds are being
fabricated out of rolled steel sections and plates can be
welded within a tolerance of 1 mm. The most important
factors in the production of a successful and economical
weldment or broken part repair is the minimization of
distortion. Excessive distortion increase the job cost due to
expense of rectification or may cause the job careless.
Thus welding deformation not only complicates the
fabrication of welded structure but also minimize its fitness
for the job for which it is designed. Moreover in welding
causes locked up stress or residual stress in the weld zone
which on one hand contributes to weld cracking and on the
other size it is suspected to have an important effect on the
brittle fracture of the welded structures. This may also
reduce the load carrying capacity of the member. Hence the
prediction of distortion and its thorough analysis is called
for.
2. EXPERIMENTAL FRAMEWORK
Though studies of distortion have been carried out by so
many authors, still there is general lack of experimental data
on different types of distortion such as transverse and
longitudinal, shrinkage, angular distortion, bowing
particularly for butt weld (v-groove) joint. However angular
distortion has been studied but effect of different welding
parameters on this type of distortion in butt weld cross-
section is not fully clarified. Moreover availability of data on
other types of distortion is so scare that verification of
theoretical prediction is difficult. Hence it is necessary to
perform some more experimental investigation on them.
So experimental were designed for measuring the
following distortion ofbutt weldjointshavingdifferenttypes
of weld details and different thickness(e.g. 6 mm, 7 mm & 8
mm ) of the plates.
1 Longitudinal shrinkage
2 Transverse shrinkage
2.1 Test plate preparation
Thirty six numbers of different thickness (e.g. 6 mm,7mm&
8 mm) test plates were cut by power hacksaw from a rolled
Indian standard plate, ISP 16, having material specification
mild steel (IS 226) and EN-8.
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 06 | June 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 3359
2.2 Photograph of the experiments
There are some photographs of EN-8 Plate of dimension
100mmX50mmX8mm. The thickness of the plates has to be
made as mentioned in the photographs.Vgroovesarealsoto
cut on these plate as mentioned in the photographs. These
pictures are taken after cutting the plates from the length of
Flat
FIG 2.1- EN-8 SPECIMEN OF DIFFERENT THICKNESS
FIG 2.2-WELDING OF EN8 PLATE
3. Results
3.1 Transverse shrinkage distortion Measurement
The values obtained for transverse shrinkage for all the
jobs i.e. P1, P2 , P3 P4 ,P5 , P6 , P7 , P8 , P9 .
TABLE 3.1- TRANSVERSE SHRINKAGE IN PLATES OF
EN-8.
Plate
thickness in
mm.
Weld
section in
degree
Average
transverse
shrinkage in
mm.
8 600 0.991
7 600 0.730
6 600 0.471
8 900 1.331
7 900 0.801
6 900 0.713
8 1200 1.803
7 1200 1.365
6 1200 1.131
3.2. Longitudinal shrinkage distortion Measurement
The values obtained for longitudinal shrinkage are given
below in Table No. 3.2 for all the work-pieces (i.e. P1 to
P9).
TABLE 3.2-TABLE OF AVERAGE LONGITUDINAL
SHRINKAGE IN PLATES OF EN-8
Plate
thickness in
mm.
Weld
section in
degree
Average
longitudinal
shrinkage in mm
8 600 1.012
7 600 0.631
6 600 0.690
8 900 1.494
7 900 1.125
6 900 1.096
8 1200 1.916
7 1200 1.741
6 1200 1.17
4. Mathematical model for the experiments
4.1 Anova testing for the distortion in EN8 plate
In the response table we take the factor 1 as the plate
thickness and factor 2 as grove angle, and two different
response as deflection andshrinkageforEN8plate.Thetable
drawn below.
TABLE 4.1 ROSPONSE TABLE FOREN8
Factor
1
Factor
2
Response 1 Response 2
A:A B:B Deflection
(EN 8)
Longitudinal
shrinkage (EN 8)
mm mm
1 0 2.2887 1.494
0 -1 2.1758 0.631
-1 1 1.5675 1.096
-1 -1 1.8518 0.69
0 0 1.9728 1.125
1 -1 2.8213 1.012
-1 0 1.7819 1.175
1 1 1.7898 1.916
0 1 1.6662 1.741
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 06 | June 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 3360
4.2 Analysis of variance Quadratic model for deflection
in EN8
TABLE 4.2- QUADRATIC MODEL TABLE
Source Sum of
Squares
F-
value
p-
value
Model 1.19 69.80 0.0027 significant
A-A 0.4809 140.94 0.0013 significant
B-B 0.5553 162.77 0.0010 significant
AB 0.1396 40.91 0.0077 significant
A² 0.0123 3.62 0.0433 significant
B² 0.0026 0.7485 0.4506 significant
Residual 0.0102
Cor
Total
1.20
Factor coding is in the form of plate thickness and groove
angle
The Model F-value of 69.80 implies the model is significant.
There is only a 0.27% chance that an F-value this largecould
occur due to noise.
P-values less than 0.0500 indicate model terms are
significant.
4.3 ONE FACTOR
1) One factor means, effect of groove angle on deflectionof
EN8. In the graph for the case of EN8 deflection increase
with the increase in groove angle. But when we take the
factor as plate thickness the deflectiondecreasewiththe
increase of plate thickness
Design-Expert® Software
Trial Version
Factor Coding: Actual
Deflection (EN 8) (mm)
X1 = A: A
Actual Factor
B: B = 0
Groove angle
-1 -0.5 0 0.5 1
Deflection(EN8)(mm)
1.4
1.6
1.8
2
2.2
2.4
2.6
2.8
3
One Factor
GRAPH4.1- PLOT FOR THE DEFLECTION IN EN8 FOR
GROOVE ANGLE VERSES DEFLECTION
Design-Expert® Software
Trial Version
Factor Coding: Actual
Deflection (EN 8) (mm)
X1 = B: B
Actual Factor
A: A = 0
Plate thickness
-1 -0.5 0 0.5 1
Deflection(EN8)(mm)
1.4
1.6
1.8
2
2.2
2.4
2.6
2.8
3
One Factor
GRAPH4.2- PLOT FOR THE DEFLECTION IN EN8 FOR
PLATE THICKNESS VERSES DEFLECTION
Design-Expert® Software
Trial Version
Factor Coding: Actual
Deflection (EN 8) (mm)
1.5675 2.8213
X1 = A: A
X2 = B: B
-1
-0.5
0
0.5
1
-1
-0.5
0
0.5
1
1.4
1.6
1.8
2
2.2
2.4
2.6
2.8
3
Deflection(EN8)(mm)
Groove anglePlate thickness
GRAPH4.3- PLOT FOR THE DEFLECTION IN EN8 FOR
GROOVE ANGLE, PLATE THICKNESS VERSES
DEFLECTION
5. CONCLUSIONS
Following conclusion are observed.
From the above tables and the graph it is very clear that for
EN8 plate when the groove angle is increasethedeflectionin
the plate is also increase, its observed from the graph that
the deflection is minimum for the notch angle 60 degree and
it is maximum for 120 degree.
From the above tables and the graph it is very clear that for
EN8 plate when the plate thickness is increasethedeflection
in the plate is decrease, its observed from the graph that the
deflection is minimumfor8MMplateand maximumfor 6MM
plate.
References
[1] C. L. Tsai, S. C. Park and W. T. Cheng, 1999, "Welding
Distortion of a Thin- Plate Panel Structure"
[2] T.D. Huang, Pingsha Dong,LawrenceA.DeCan,Dennis
D.Harwig, 2003, "Residual stresses and Distortions in
Light weight ship panel structures".
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 06 | June 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 3361
[3] V. VEL MURUGAN AND V. GUNARAJ, 2005," Effects of
Process Parameters on Angular Distortion of Gas Metal
Arc Welded Structural Steel Plates", Sponsored by the
American Welding Society and the Welding Research
Council
[4] Dean Deng,2008," FEM predictionofweldingresidual
stress and distortion in carbon steel considering phase
transformation effects", Research Centre of
Computational Mechanics Inc., Department of Technical
Development, Togoshi NI-Building, 1-7-1, Togoshi,
Shinagawa-ku,Tokyo 142-0041, Japan.
[5] S.F. Estefen , T. Gurova , X. Castello , A. Leontiev, 2009,
"Surface residual stress evaluation in double-electrode
butt welded steel plates"
[6] De-An DENG,2010," Theoretical predictionof welding
distortion in large and complex structures", College of
Material Science and Engineering, Chongqing University,
Chongqing 400045, China.
[7] Panagiotis Michaleris and Andrew DeBiccari,
"Prediction of Welding Distortion", Edison Welding
Institute Columbus, Ohio.
[8] Dean Deng, Ninshu Ma, Hidekazu Murakawa, "Finite
element analysis of welding distortion in a large thin
plate panel structure", Transaction of JWRI, Vol.
40(2011), No.1.
[9] B. N. Sathyanarayana Reddy and N. Lakshmana
Swamy, 2013, "Influence of Groove Angle in V-groove
Butt joints on Transverse shrinkage in CO2 Arc Welding
process", Research Scholar, Dept. of Mech. Engg., UVCE,
Bangalore University, Bangalore, Karnataka, INDIA,
Professor, Dept. of Mech. Engg., UVCE, Bangalore
University, Bangalore, Karnataka, INDIA, respectively.
[10] R.R. Chand , I.S. Kim , J.P. Lee, Y.S. Kim , D.G. Kim,
2013, "Numerical andexperimentstudyofresidual stress
and strain in multi-pass GMA welding".
[11] h.long, d.grey, a.carlier, p.g.maropoulos, 2014,
"prediction of welding distortion in butt joint of thin
plates".
[12] tapas bajpei, h. Chelladurai, m. Zahid ansari,
experimental investigation and numerical analyses of
residual stresses and distortions in gma welding of thin
dissimilar aa5052-aa6061 plates, 2017
[13] chunbiao wu, jae-woong kim, analysis of welding
residual stress formation behavior during
circumferential tig welding of a pipe, 2018

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Distortion in EN-8 Plates of Varying Thickness and Cross-Sections

  • 1. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 06 | June 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 3358 DISTORTION IN EN-8 PLATES HAVING DIFFERENT THICKNESS AND CROSS SECTIONS USING MANUAL ELECTRIC ARC WELDING ABHAY KUMAR MISHRA1, VIKAS KUMAR SHUKLA2, RATI SALUJA3 1M.Tech research scholar, GITM, Lucknow, UP, India 2Assistant Professor Dept. of Mechanical Engineering, GITM, Lucknow, UP, India 3P.hd research scholar, Dept. of Mechanical Engineering, Integral University, Lucknow, UP, India ---------------------------------------------------------------------***---------------------------------------------------------------------- Abstract - Welding is a process of joining two or more similar or dissimilar material with the application of heat with or without the application of filler material and pressure in which heat is supplied either electrically or by means of a gas torch. Welding is an important process for fabrication of engineering components. It has vast applications in ship buildings, constructions, aerospace, automobile industries, etc. There are different welding defects due to which weldments fails under service conditions and cause damage to the property and loss of human lives. In this work we are going to study one of the most important welding defects known as Distortion. Distortion is the change in shape and variation between the positions of the two plates before welding andafter welding. Distortion occurs due to good amount of temperature difference at different points along the joint and thus at any instant certain area of base metal expands and other including weld bead contract. In this work we are going to study how much distortion occur in medium carbon steel that is EN-8 Plates of various cross-sections and thickness. This study is done by experiment and justify the result using ANOVA. Key Words: Distortion, Mild Steel, EN-8, Butt Joint, Arc Welding & Single V Groove, ANOVA 1. INTRODUCTION OF DISTORTION The term distortion means deviation from desired or actual shape and size. In welding terminology distortionmeansthe local residual deformation resulting from welding which changes the dimension and shape of the work-piece joined. While doing welding when the welding operator used eye shield and electrode holder, commenced welding a job, starting and finishing at any place. After completion of the job if it was found distorted and it was taken forgrantedthat it could not be avoided. The impression was all welding caused distortion. That why think of it. This was purely ignorance, because distortion can be controlled and minimized by approaching the job holding in the correct manner. At present era, welding can be done with minimum distortion. For example, different machines beds are being fabricated out of rolled steel sections and plates can be welded within a tolerance of 1 mm. The most important factors in the production of a successful and economical weldment or broken part repair is the minimization of distortion. Excessive distortion increase the job cost due to expense of rectification or may cause the job careless. Thus welding deformation not only complicates the fabrication of welded structure but also minimize its fitness for the job for which it is designed. Moreover in welding causes locked up stress or residual stress in the weld zone which on one hand contributes to weld cracking and on the other size it is suspected to have an important effect on the brittle fracture of the welded structures. This may also reduce the load carrying capacity of the member. Hence the prediction of distortion and its thorough analysis is called for. 2. EXPERIMENTAL FRAMEWORK Though studies of distortion have been carried out by so many authors, still there is general lack of experimental data on different types of distortion such as transverse and longitudinal, shrinkage, angular distortion, bowing particularly for butt weld (v-groove) joint. However angular distortion has been studied but effect of different welding parameters on this type of distortion in butt weld cross- section is not fully clarified. Moreover availability of data on other types of distortion is so scare that verification of theoretical prediction is difficult. Hence it is necessary to perform some more experimental investigation on them. So experimental were designed for measuring the following distortion ofbutt weldjointshavingdifferenttypes of weld details and different thickness(e.g. 6 mm, 7 mm & 8 mm ) of the plates. 1 Longitudinal shrinkage 2 Transverse shrinkage 2.1 Test plate preparation Thirty six numbers of different thickness (e.g. 6 mm,7mm& 8 mm) test plates were cut by power hacksaw from a rolled Indian standard plate, ISP 16, having material specification mild steel (IS 226) and EN-8.
  • 2. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 06 | June 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 3359 2.2 Photograph of the experiments There are some photographs of EN-8 Plate of dimension 100mmX50mmX8mm. The thickness of the plates has to be made as mentioned in the photographs.Vgroovesarealsoto cut on these plate as mentioned in the photographs. These pictures are taken after cutting the plates from the length of Flat FIG 2.1- EN-8 SPECIMEN OF DIFFERENT THICKNESS FIG 2.2-WELDING OF EN8 PLATE 3. Results 3.1 Transverse shrinkage distortion Measurement The values obtained for transverse shrinkage for all the jobs i.e. P1, P2 , P3 P4 ,P5 , P6 , P7 , P8 , P9 . TABLE 3.1- TRANSVERSE SHRINKAGE IN PLATES OF EN-8. Plate thickness in mm. Weld section in degree Average transverse shrinkage in mm. 8 600 0.991 7 600 0.730 6 600 0.471 8 900 1.331 7 900 0.801 6 900 0.713 8 1200 1.803 7 1200 1.365 6 1200 1.131 3.2. Longitudinal shrinkage distortion Measurement The values obtained for longitudinal shrinkage are given below in Table No. 3.2 for all the work-pieces (i.e. P1 to P9). TABLE 3.2-TABLE OF AVERAGE LONGITUDINAL SHRINKAGE IN PLATES OF EN-8 Plate thickness in mm. Weld section in degree Average longitudinal shrinkage in mm 8 600 1.012 7 600 0.631 6 600 0.690 8 900 1.494 7 900 1.125 6 900 1.096 8 1200 1.916 7 1200 1.741 6 1200 1.17 4. Mathematical model for the experiments 4.1 Anova testing for the distortion in EN8 plate In the response table we take the factor 1 as the plate thickness and factor 2 as grove angle, and two different response as deflection andshrinkageforEN8plate.Thetable drawn below. TABLE 4.1 ROSPONSE TABLE FOREN8 Factor 1 Factor 2 Response 1 Response 2 A:A B:B Deflection (EN 8) Longitudinal shrinkage (EN 8) mm mm 1 0 2.2887 1.494 0 -1 2.1758 0.631 -1 1 1.5675 1.096 -1 -1 1.8518 0.69 0 0 1.9728 1.125 1 -1 2.8213 1.012 -1 0 1.7819 1.175 1 1 1.7898 1.916 0 1 1.6662 1.741
  • 3. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 06 | June 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 3360 4.2 Analysis of variance Quadratic model for deflection in EN8 TABLE 4.2- QUADRATIC MODEL TABLE Source Sum of Squares F- value p- value Model 1.19 69.80 0.0027 significant A-A 0.4809 140.94 0.0013 significant B-B 0.5553 162.77 0.0010 significant AB 0.1396 40.91 0.0077 significant A² 0.0123 3.62 0.0433 significant B² 0.0026 0.7485 0.4506 significant Residual 0.0102 Cor Total 1.20 Factor coding is in the form of plate thickness and groove angle The Model F-value of 69.80 implies the model is significant. There is only a 0.27% chance that an F-value this largecould occur due to noise. P-values less than 0.0500 indicate model terms are significant. 4.3 ONE FACTOR 1) One factor means, effect of groove angle on deflectionof EN8. In the graph for the case of EN8 deflection increase with the increase in groove angle. But when we take the factor as plate thickness the deflectiondecreasewiththe increase of plate thickness Design-Expert® Software Trial Version Factor Coding: Actual Deflection (EN 8) (mm) X1 = A: A Actual Factor B: B = 0 Groove angle -1 -0.5 0 0.5 1 Deflection(EN8)(mm) 1.4 1.6 1.8 2 2.2 2.4 2.6 2.8 3 One Factor GRAPH4.1- PLOT FOR THE DEFLECTION IN EN8 FOR GROOVE ANGLE VERSES DEFLECTION Design-Expert® Software Trial Version Factor Coding: Actual Deflection (EN 8) (mm) X1 = B: B Actual Factor A: A = 0 Plate thickness -1 -0.5 0 0.5 1 Deflection(EN8)(mm) 1.4 1.6 1.8 2 2.2 2.4 2.6 2.8 3 One Factor GRAPH4.2- PLOT FOR THE DEFLECTION IN EN8 FOR PLATE THICKNESS VERSES DEFLECTION Design-Expert® Software Trial Version Factor Coding: Actual Deflection (EN 8) (mm) 1.5675 2.8213 X1 = A: A X2 = B: B -1 -0.5 0 0.5 1 -1 -0.5 0 0.5 1 1.4 1.6 1.8 2 2.2 2.4 2.6 2.8 3 Deflection(EN8)(mm) Groove anglePlate thickness GRAPH4.3- PLOT FOR THE DEFLECTION IN EN8 FOR GROOVE ANGLE, PLATE THICKNESS VERSES DEFLECTION 5. CONCLUSIONS Following conclusion are observed. From the above tables and the graph it is very clear that for EN8 plate when the groove angle is increasethedeflectionin the plate is also increase, its observed from the graph that the deflection is minimum for the notch angle 60 degree and it is maximum for 120 degree. From the above tables and the graph it is very clear that for EN8 plate when the plate thickness is increasethedeflection in the plate is decrease, its observed from the graph that the deflection is minimumfor8MMplateand maximumfor 6MM plate. References [1] C. L. Tsai, S. C. Park and W. T. Cheng, 1999, "Welding Distortion of a Thin- Plate Panel Structure" [2] T.D. Huang, Pingsha Dong,LawrenceA.DeCan,Dennis D.Harwig, 2003, "Residual stresses and Distortions in Light weight ship panel structures".
  • 4. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 06 | June 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 3361 [3] V. VEL MURUGAN AND V. GUNARAJ, 2005," Effects of Process Parameters on Angular Distortion of Gas Metal Arc Welded Structural Steel Plates", Sponsored by the American Welding Society and the Welding Research Council [4] Dean Deng,2008," FEM predictionofweldingresidual stress and distortion in carbon steel considering phase transformation effects", Research Centre of Computational Mechanics Inc., Department of Technical Development, Togoshi NI-Building, 1-7-1, Togoshi, Shinagawa-ku,Tokyo 142-0041, Japan. [5] S.F. Estefen , T. Gurova , X. Castello , A. Leontiev, 2009, "Surface residual stress evaluation in double-electrode butt welded steel plates" [6] De-An DENG,2010," Theoretical predictionof welding distortion in large and complex structures", College of Material Science and Engineering, Chongqing University, Chongqing 400045, China. [7] Panagiotis Michaleris and Andrew DeBiccari, "Prediction of Welding Distortion", Edison Welding Institute Columbus, Ohio. [8] Dean Deng, Ninshu Ma, Hidekazu Murakawa, "Finite element analysis of welding distortion in a large thin plate panel structure", Transaction of JWRI, Vol. 40(2011), No.1. [9] B. N. Sathyanarayana Reddy and N. Lakshmana Swamy, 2013, "Influence of Groove Angle in V-groove Butt joints on Transverse shrinkage in CO2 Arc Welding process", Research Scholar, Dept. of Mech. Engg., UVCE, Bangalore University, Bangalore, Karnataka, INDIA, Professor, Dept. of Mech. Engg., UVCE, Bangalore University, Bangalore, Karnataka, INDIA, respectively. [10] R.R. Chand , I.S. Kim , J.P. Lee, Y.S. Kim , D.G. Kim, 2013, "Numerical andexperimentstudyofresidual stress and strain in multi-pass GMA welding". [11] h.long, d.grey, a.carlier, p.g.maropoulos, 2014, "prediction of welding distortion in butt joint of thin plates". [12] tapas bajpei, h. Chelladurai, m. Zahid ansari, experimental investigation and numerical analyses of residual stresses and distortions in gma welding of thin dissimilar aa5052-aa6061 plates, 2017 [13] chunbiao wu, jae-woong kim, analysis of welding residual stress formation behavior during circumferential tig welding of a pipe, 2018