Memoria Investigaciones en Ingeniería, núm. 30 (2026). pp. 30-55
https://doi.org/10.36561/ING.30.4
ISSN 2301-1092 ISSN (en línea) 2301-1106 Universidad de Montevideo, Uruguay
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30
Thermo-Mechanical FEM Study of SMAW Parameter Effects in S355J2+N /
ASTM A572 Gr.50 Dissimilar Steel Joints
Estudio termomecánico mediante el método de elementos finitos de los efectos de
los parámetros de la soldadura SMAW en uniones de aceros disímiles S355J2+N /
ASTM A572 Gr.50.
Estudo termomecânico por elementos finitos dos efeitos dos parâmetros de
soldagem SMAW em juntas de aços dissimilares S355J2+N / ASTM A572 Gr.50
Syed Farrukh Haider
1
, Shaheryar A. Khan
2
(*), Aqueel Shah
3
, Muhammad Nasir Bashir
4
, Asif Mansoor
5
,
Abbas Hussain
6
, M. Mahmood Ali
7
, Salman Nisar
8
Recibido: 09/09/2025 Aceptado: 24/11/2025
Summary. - Shielded Metal Arc Welding (SMAW) is widely employed in structural steel fabrication; however, the
thermo-mechanical response of dissimilar structural steel joints remains insufficiently explored through numerical
modeling. In this study, a three-dimensional transient thermo-mechanical finite element model is developed to
investigate SMAW of dissimilar S355J2+N and ASTM A572 Grade 50 steel plates. Goldak’s double-ellipsoidal heat
source is implemented to represent arc heat input, and a BoxBehnken design is employed to systematically examine
the influence of welding current, voltage, and travel speed. The analysis focuses on peak temperature, out-of-plane
distortion, and elastic stress indicators derived from a linear thermo-elastic formulation. The results indicate that
welding current predominantly governs peak temperature, while travel speed has the strongest influence on thermal
gradients and distortion behavior; voltage exhibits a secondary but non-negligible effect on heat distribution. Simulated
thermal and deformation trends are benchmarked against published experimental and numerical studies on comparable
structural steels and show consistent qualitative behavior. Owing to the absence of plasticity, temperature-dependent
material properties, and direct experimental validation, stress results are interpreted solely as qualitative indicators
rather than physically realistic residual stresses. The study provides a structured thermo-elastic FEM and design-of-
experimentsbased sensitivity framework for a dissimilar structural steel combination not previously reported in
SMAW numerical studies, offering practical insight into parameter screening for thermal and distortion control in
structural steel fabrication.
(*) Corresponding author.
1
Postgraduate Student, National University of Sciences and Technology (Pakistan), syedhaider270@yahoo.com,
ORCID iD: https://orcid.org/0009-0007-2560-2664
2
Associate Professor and Head of the Department of Mechanical Engineering., DHA Suffa University (Pakistan), shaheryar.atta@dsu.edu.pk,
ORCID iD: https://orcid.org/0000-0003-1600-7322
3
Professor, National University of Sciences and Technology (Pakistan), a.shah@smme.nust.edu.pk,
ORCID iD: https://orcid.org/0000-0002-4845-9350
4
Assistant Professor, National University of Sciences and Technology (Pakistan), mnasir@ceme.nust.edu.pk,
ORCID iD: https://orcid.org/0000-0001-9620-5980
5
Assistant Professor, National University of Sciences and Technology (Pakistan), asif.mansure@pnec.nust.edu.pk,
ORCID iD: https://orcid.org/0000-0002-2127-0961
6
Assistant Professor, National University of Sciences and Technology (Pakistan), abbas.hussain@pnec.nust.edu.pk,
ORCID iD: https://orcid.org/0009-0008-1680-6507
7
Lecturer, Atlantic Technological University (Ireland), Muhammad.Ali@atu.ie,
ORCID iD: https://orcid.org/0000-0001-8236-2459
8
Assistant Professor, Taibah University (Kingdom of Saudi Arabia), snahmed@taibahu.edu.sa,
ORCID iD: https://orcid.org/0009-0008-1680-6507
S. F. Haider, S. A. Khan, A. Shah, M. N. Bashir, A. Mansoor, A. Hussain, M. M. Ali, S. Nisar
Memoria Investigaciones en Ingeniería, núm. 30 (2026). pp. 30-55
https://doi.org/10.36561/ING.30.4
ISSN 2301-1092 ISSN (en línea) 2301-1106 Universidad de Montevideo, Uruguay
31
Keywords: Finite Element Method (FEM); Goldak’s double ellipsoidal model; SMAW; Solid Mechanics; Thermal
distribution.
Resumen. - La soldadura por arco metálico protegido (SMAW) se emplea ampliamente en la fabricación de acero
estructural; sin embargo, la respuesta termomecánica de las uniones de aceros estructurales disímiles aún no se ha
explorado suficientemente mediante modelado numérico. En este estudio, se desarrolla un modelo tridimensional
transitorio termomecánico de elementos finitos para investigar la SMAW de placas de acero disímiles S355J2+N y
ASTM A572 Grado 50. Se implementa la fuente de calor elipsoidal doble de Goldak para representar el aporte de
calor del arco, y se emplea un diseño Box-Behnken para examinar sistemáticamente la influencia de la corriente de
soldadura, el voltaje y la velocidad de avance. El análisis se centra en la temperatura máxima, la distorsión fuera del
plano y los indicadores de tensión elástica derivados de una formulación termoelástica lineal. Los resultados indican
que la corriente de soldadura rige predominantemente la temperatura máxima, mientras que la velocidad de avance
tiene la mayor influencia en los gradientes térmicos y el comportamiento de distorsión; el voltaje exhibe un efecto
secundario, pero no despreciable, en la distribución del calor. Las tendencias térmicas y de deformación simuladas se
comparan con estudios experimentales y numéricos publicados sobre aceros estructurales comparables y muestran un
comportamiento cualitativo consistente. Debido a la ausencia de plasticidad, propiedades del material dependientes
de la temperatura y validación experimental directa, los resultados de tensión se interpretan únicamente como
indicadores cualitativos, en lugar de tensiones residuales físicamente realistas. Este estudio proporciona un marco de
sensibilidad termoelástico estructurado basado en el método de elementos finitos (MEF) y el diseño de experimentos
para una combinación de aceros estructurales diferentes, no reportada previamente en estudios numéricos de
soldadura por arco con electrodo revestido (SMAW). Esto ofrece información práctica para la selección de parámetros
para el control térmico y de distorsión en la fabricación de acero estructural.
Palabras clave: Método de elementos finitos (MEF); Modelo elipsoidal doble de Goldak; SMAW; Mecánica de sólidos;
Distribución térmica.
Resumo. - A soldagem a arco com eletrodo revestido (SMAW) é amplamente empregada na fabricação de aço
estrutural; no entanto, a resposta termomecânica de juntas de o estrutural dissimilares permanece insuficientemente
explorada por meio de modelagem numérica. Neste estudo, um modelo tridimensional transiente de elementos finitos
termomecânicos é desenvolvido para investigar a soldagem a arco com eletrodo revestido de chapas de aço
dissimilares S355J2+N e ASTM A572 Grau 50. A fonte de calor de duplo elipsoide de Goldak é implementada para
representar a entrada de calor do arco, e um planejamento Box-Behnken é empregado para examinar sistematicamente
a influência da corrente de soldagem, da tensão e da velocidade de deslocamento. A análise concentra-se na
temperatura máxima, na distorção fora do plano e nos indicadores de tensão elástica derivados de uma formulação
termoelástica linear. Os resultados indicam que a corrente de soldagem governa predominantemente a temperatura
máxima, enquanto a velocidade de deslocamento tem a influência mais forte nos gradientes térmicos e no
comportamento de distorção; a tensão apresenta um efeito secundário, mas não desprezível, na distribuição de calor.
As tendências térmicas e de deformação simuladas são comparadas com estudos experimentais e numéricos publicados
sobre os estruturais comparáveis e mostram um comportamento qualitativo consistente. Devido à ausência de
plasticidade, propriedades do material dependentes da temperatura e validação experimental direta, os resultados de
tensão são interpretados apenas como indicadores qualitativos, em vez de tensões residuais fisicamente realistas. O
estudo fornece uma estrutura de sensibilidade termoelástica baseada no método dos elementos finitos (MEF) e no
planejamento de experimentos para uma combinação de aços estruturais distintos, não relatada anteriormente em
estudos numéricos de soldagem com eletrodo revestido (SMAW), oferecendo informações práticas sobre a seleção de
parâmetros para o controle térmico e de distorção na fabricação de aço estrutural.
Palavras-chave: Método dos Elementos Finitos (MEF); Modelo elipsoidal duplo de Goldak; SMAW; Mecânica dos
Sólidos; Distribuição térmica.
S. F. Haider, S. A. Khan, A. Shah, M. N. Bashir, A. Mansoor, A. Hussain, M. M. Ali, S. Nisar
Memoria Investigaciones en Ingeniería, núm. 30 (2026). pp. 30-55
https://doi.org/10.36561/ING.30.4
ISSN 2301-1092 ISSN (en línea) 2301-1106 Universidad de Montevideo, Uruguay
32
1. Introduction. - Welding is one of the most widely used fabrication processes for permanently joining metallic
components in structural, pressure vessel, shipbuilding, and repair applications. In fusion welding processes, the joint
is formed by localized melting of the base (parent) material with or without the addition of a consumable filler metal,
followed by solidification to create a welded joint or weldment [1], [2]. The selection of welding consumables is
typically guided by compatibility with the parent materials in order to achieve acceptable metallurgical integrity and
mechanical performance of the joint.
Among conventional arc welding techniques, Shielded Metal Arc Welding (SMAW), also referred to as stick welding,
remains one of the most versatile and widely adopted processes due to its simplicity, portability, and applicability in
both indoor and outdoor environments. SMAW is extensively employed in construction, shipbuilding, maintenance,
and repair industries. In this process, an electric arc is established between a flux-coated consumable electrode and the
workpiece, generating the heat required for melting the base metal and filler material. The decomposition of the flux
coating produces shielding gases and slag, which protect the molten weld pool from atmospheric contamination such
as oxygen and hydrogen, thereby reducing defects such as porosity and cracking [24]. A schematic representation of
the SMAW process and its associated heat source modeling framework is shown in Fig. 1. The figure illustrates the
interaction between the welding arc, consumable electrode, base metals, and the implementation of the moving heat
source within the finite element domain.
Figure I. Schematic representation of the Shielded Metal Arc Welding (SMAW) process and numerical modeling
framework adopted in the present study. [4].
Despite its widespread industrial use, SMAW involves highly localized and transient thermal cycles that induce steep
temperature gradients within the weldment. These thermal gradients, in turn, govern the evolution of microstructure,
distortion, and residual stresses, which critically influence the dimensional accuracy and service performance of welded
components. As a result, understanding the influence of welding parameters, such as current, voltage, and travel speed,
on thermal and mechanical responses remains a central concern in welding science and engineering.
In recent decades, finite element modeling (FEM) has emerged as a powerful tool for analyzing welding processes,
offering detailed insight into transient temperature fields, deformation behavior, and stress development that are
difficult to measure experimentally. Numerous studies have investigated the effects of welding parameters on similar
and dissimilar materials using both experimental and numerical approaches.
Table I summarizes representative experimental and numerical studies investigating the influence of welding
parameters on thermal, mechanical, and metallurgical responses for various arc welding processes and materials [4
40].
S. F. Haider, S. A. Khan, A. Shah, M. N. Bashir, A. Mansoor, A. Hussain, M. M. Ali, S. Nisar
Memoria Investigaciones en Ingeniería, núm. 30 (2026). pp. 30-55
https://doi.org/10.36561/ING.30.4
ISSN 2301-1092 ISSN (en línea) 2301-1106 Universidad de Montevideo, Uruguay
33
Author(s)
Welding Process
Material
Findings
1
M. E. Aalami-Aleagha et al
[4]
SMAW
Steel pipe API
5L grade
Moderate Current produced optimum hardness.
2
Hunchul Jeong et al. [5]
GTAW
Aluminum
A16061
reverse polarity produced more heat input than
straight polarity.
3
Chao Wang et al. [6]
GMAW
SM400A
Residual stresses more with welding increased
local heating and cutting.
4
Dong Ho Bae et al. [7]
GTAW
SUS304L
Longitudnal Residual Stress = 300 MPa; wider
stress zones obtained with double ellipsoid model
than ramp heat input model.
5
Chang-Sung Seok et al. [8]
MIG
High tensile
steel H-plate
Maximum tensile residual stress found at center
of thickness.
6
Chang-Sung Seok et al. [9]
GMAW
Steel Pipe
C-seam weldment on pipe produced larger
longitudinal bending deformation than the L-
seam pipe.
7
Dong-Yoon Kim et al. [10]
GMAW
Hot press
forming steel
sheets
Low Wire feed speed produced and current
produced high tensile strength.
8
Yong Hua Shi et al. [11]
K-TIG
Q345
Segmentation LSTM Model has 95.2% accuracy
to recognize the weld penetration state.
9
Zeng Liu et al. [12]
GMAW
High nitrogen
and martensitic
low alloy steel
ER 307Mo filler metal produced lower porosity
and optimum joint strength as compared to ER
2209 and ER 120 S-G.
10
M. Mazar Atabaki et al. [13]
HLAW
High strength
quenched and
tempered steel
Stand-off distance had more impact on weld
quality and penetration as compared to welding
speed and power.
11
Qiang Lang et al. [14]
TIG
Transformation
induced
plasticity (TRIP)
Steel
Addition of Laser to low current TIG increased
weld depth and changed the fracture form from
brittle to ductile.
12
Guoqing Wu et al. [15]
Tungsten-Argon
Welding
LA141 alloy
plates
With argon protection device and homogenous
welding wires, the tensile strength increased to
124 MPa i.e 95% of base metal and
microhardness improved.
13
A. G. Kamble et al. [16]
GMAW
AISI 321 SS
plates
Bead penetration is increased with an increase in
speed, gas flow rate, and wire feed rate.
14
Rohit Jha et al. [17]
TIG
MS
Maximum tensile strength at the highest current
of 110 A and a welding speed of 157.80 mm/min.
15
Afnan Dadi et al. [18]
SMAW
MS SA-516 Gr.
70
Highest tensile strength obtained at a current of
120 A.
16
R. A. Mohammed et al. [19]
SMAW
Medium Carbon
Steel
Highest hardness and tensile strength but lower
impact strength obtained at HAZ than weldment
and parent metal.
17
Brijesh Sharma et al. [20]
SMAW and
GMAW
MS 2062
Maximum penetration and optimum bead
obtained with SMAW, at current = 100 A,
voltage = 24 V and arc length = 3mm, as
compared to GMAW.
18
Asibeluo et al. [21]
SMAW
A-36 steel
Highest hardness of 114 HB was obtained at
lowest current of 70 A.
19
J.O. Olawale et al [22]
SMAW
Low carbon steel
Increase in current increased the tensile strength
and hardness but reduced impact strength.
20
Abhishek Shukla et al. [23]
SMAW
AISI 1020
RSM and experimental results are closer and
maximum current of 120 A provided the highest
tensile strength of 259 MPa.
S. F. Haider, S. A. Khan, A. Shah, M. N. Bashir, A. Mansoor, A. Hussain, M. M. Ali, S. Nisar
Memoria Investigaciones en Ingeniería, núm. 30 (2026). pp. 30-55
https://doi.org/10.36561/ING.30.4
ISSN 2301-1092 ISSN (en línea) 2301-1106 Universidad de Montevideo, Uruguay
34
Table I. Examples of welding parameters' effect on Steel Specimen from Literature.
21
Randy Chiong et al. [24]
SMAW
AISI 1018
Maximum hardness and tensile strength, 452
MPa and 195 HV, respectively, obtained at
highest current.
22
Deepak Pathak et al. [25]
SMAW
Low carbon steel
Highest tensile strength observed at DCEN
polarity and highest current.
23
S.H. Zoalfakar et al. [26]
SMAW
ST 37/2, ST
44/2, and ST
52/3 steel plates
Increasing Carbon equivalent (C.E) % and
groove angle, increased the tensile strength and
hardness.
24
Edi Widodo et al. [27]
SMAW
SS AISI 304
Highest tensile strength of 632 MPa obtained at
highest current of 90 A.
25
Dhananjay Kumar et al. [28]
TIG and SMAW
SS 304L
Distortion of TIG was lesser as compared to
SMAW.
26
A.K. Rude et al. [29]
SMAW
MS
Micro hardness decreases with increase in
welding current but increases with number of
layers.
27
Rajiv Selvam et al. [30]
SMAW
Carbon steel
pipes
E- 6010 and E-7018 filler metals produced
greater hardness, ductility, and toughness as
compared to E-7010 and E-7018.
28
L. S. Sisira K
Weerasekralage et al. [31]
SMAW
MS
Highest weldment quality obtained with current
of 123 A, voltage of 27 V, and 60 º included
angle.
29
Digambar Benne et al. [32]
SMAW
MS
With increase in current, voltage, and speed, the
hard-faced part’s hardness and impact strength
was increased.
30
Talabi et al. [33]
SMAW
Low carbon steel
Increase in current and voltage increased the
tensile strength and yield strength but reduced the
hardness.
31
U.S. Patil et al. [34]
SMAW
SS 304 and MS
1018
With the current = 85 A, welding speed = 8 mm/s,
electrode angle of 30 º, and root gap of 0.75 mm.
the highest tensile strength of 403 N/ is
obtained.
32
Mahmud Khan et al.[35]
SMAW and TIG
SS AISI 304 and
MS AISI 1020
TIG produced the highest tensile strength, %
elongation and yield strength as compared to
SMAW.
33
Mauricio Andres Rojas Nova
et al. [36]
SMAW
A 36 Steel
Increase in travel speed decreases the maximum
temperature. Optimum welding speed is obtained
when temperature of source produces
temperature just above the melting point of base
metal.
34
M Matuszewski [37]
TIG and MIG
Aluminum alloy
6060 sheet
TIG with argon shielded with addition of metallic
wire; MIG determined the fusion zone of sheets.
35
Sajeeb A.M. [38]
TIG
Aluminum alloy
6061-T6
Weld penetration was increased by increase in
current and deacrease in stand-off distance.
Current is found to be the most significant
parameter.
36
A. Boudiaf et al. [39]
GTAW
AISI 316L
The highest temperature was observed at the
ceneter of the source; 2D model is closer to
experminetal results.
37
Cronje M [40]
SMAW
MS
Maximum distortion observed at the edge of
geometry due to less heat dissipation and
decreasing heat sink effect.
S. F. Haider, S. A. Khan, A. Shah, M. N. Bashir, A. Mansoor, A. Hussain, M. M. Ali, S. Nisar
Memoria Investigaciones en Ingeniería, núm. 30 (2026). pp. 30-55
https://doi.org/10.36561/ING.30.4
ISSN 2301-1092 ISSN (en línea) 2301-1106 Universidad de Montevideo, Uruguay
35
Across these studies, welding current is consistently reported as the dominant parameter governing heat input, with
higher currents leading to increased peak temperatures, deeper penetration, and enhanced hardness or tensile strength
in carbon and structural steels [4, 14, 1824, 33]. Welding voltage primarily influences arc stability and bead geometry,
indirectly affecting thermal distribution and residual stress development [3, 17, 20]. In contrast, welding travel speed
is repeatedly shown to act as a controlling parameter for heat input density, where increased speed reduces peak
temperature, limits fusion zone width, and mitigates distortion and residual stress accumulation [25, 33, 37, 40]. Several
studies further highlight that excessive heat input, while improving penetration, can adversely increase distortion and
tensile residual stresses, emphasizing the need for balanced parameter selection [6, 9, 28]. Despite these advances, the
majority of reported investigations focus on similar material joints or experimental optimization, with comparatively
fewer studies addressing three-dimensional transient thermo-mechanical modeling of dissimilar structural steel welds
using systematic DOE-based sensitivity analysis.
However, a careful examination of the existing literature reveals two important gaps. First, while extensive work exists
on SMAW of carbon steels, stainless steels, and aluminum alloys, numerical investigations focusing specifically on
dissimilar structural steel combinations remain limited. Second, although response surface methodologies (RSM) and
design of experiments (DOE) techniques have been successfully applied to welding processes, their integration with
three-dimensional transient thermo-mechanical FEM for SMAW remains relatively underexplored, particularly for
dissimilar steel joints.
Notably, to the best of our knowledge, no prior numerical study has reported on SMAW welding between S355J2+N
and ASTM A572 Grade 50 structural steel plates, despite the widespread industrial use of both materials in load-bearing
applications. These steels are commonly employed in construction and infrastructure projects, where dimensional
stability and thermal distortion control are critical. Understanding the sensitivity of their thermo-mechanical response
to welding parameters is therefore of practical importance.
In this study, a three-dimensional transient thermo-mechanical finite element model of the SMAW process for
dissimilar S355J2+N / ASTM A572 Gr.50 steel plates is developed using COMSOL Multiphysics. Goldak’s double-
ellipsoidal heat source formulation is employed to represent the arc heat input. A BoxBehnken design (BBD) is
adopted to systematically investigate the effects of welding current, voltage, and travel speed on key response variables,
namely maximum temperature, distortion, and elastic stress indicators. Regression and analysis of variance (ANOVA)
techniques are used to quantify the relative influence of process parameters and to identify dominant trends in the
thermo-mechanical response.
The novelty of the present work does not lie in proposing a new welding model, but rather in providing a systematic
thermo-elastic and DOE-based sensitivity assessment for a dissimilar structural steel joint that has not been previously
reported in SMAW numerical studies. The results offer quantitative insight into the relative importance of welding
parameters on thermal and distortion behavior, thereby providing a parameter-screening framework that can assist in
distortion control and process planning for structural steel fabrication.
2. Research Methodology.
2.1 Materials Selection and Geometry. - There are two different materials in this research for welding simulation
which include S355J2+N and ASTM A572 Gr.50 structural steel plates. The filler material has been assumed to be one
of the base metals i.e., S355J2+N. Table II shows the material properties and chemical composition of metals. The
material properties were adopted from published literature and standard material databases commonly used in
numerical welding simulations [36], [37], [40]. The thermal conductivity and specific heat capacity were adopted from
the standard steel material library available in COMSOL Multiphysics and commonly used literature sources. At the
same time, density values were taken from experimentally reported ranges for the selected steels. In the present study,
all thermal and mechanical properties were assumed to be temperature-independent. This simplification was adopted
to focus on the comparative influence of welding parameters on thermal distribution and deformation, while
S. F. Haider, S. A. Khan, A. Shah, M. N. Bashir, A. Mansoor, A. Hussain, M. M. Ali, S. Nisar
Memoria Investigaciones en Ingeniería, núm. 30 (2026). pp. 30-55
https://doi.org/10.36561/ING.30.4
ISSN 2301-1092 ISSN (en línea) 2301-1106 Universidad de Montevideo, Uruguay
36
maintaining reasonable computational efficiency. Although temperature-dependent properties are known to influence
residual stress development, their inclusion was beyond the scope of the current thermo-elastic framework.
Material
Chemical Composition
Young’s
Modulus
(GPa)
Density (

󰇜
Poison ratio
C
Mn
P
S
Si
S355J2+N
200
7700 to 8030
0.3
0.22
1.60
0.035
0.035
0.55
ASTM
A572 Gr. 50
190 - 210
7800
0.27-0.30
0.23
1.35
0.030
1.03
0.40
Table II. Material Properties and Chemical Composition of Metals.
The joint geometry of the dissimilar metals is shown in Figure 2. As per ISO-9692, the joint preparation of structural
steel plates was carried out on AutoCAD 2021 and 3D design was made on SolidWorks 2016.
The 2D model was designed keeping in view the recommended root gap, root face, material thickness, and bevel angle.
(Figures II(a) and II(b)) shows that the geometry consists of a root gap of 3 mm, a root face of 3 mm, and an included
angle of 60 °. The dimensions are given in millimeters.
Figure II. Three-dimensional finite element model of the dissimilar S355J2+N / ASTM A572 Gr.50 butt joint used for
thermo-mechanical simulation. [43]
2.2 Heat Source Modelling. - The current simulation work involves the use of Goldak’s double ellipsoidal heat source
model for simulating the SMAW process to provide a real-life experimental experience. This model is based on the
Gaussian distribution of power density and offers versatility to both deep and shallow penetration welds. The heat
source model has a steeper thermal gradient at the front and slightly steeper at the rear side of the ellipsoid [44], [45].
In cartesian coordinates, the power density distribution for the front and rear is given as follows [46]:
The distribution for the front quadrant:
󰇛󰇜
 
󰇛󰇜
[1]
S. F. Haider, S. A. Khan, A. Shah, M. N. Bashir, A. Mansoor, A. Hussain, M. M. Ali, S. Nisar
Memoria Investigaciones en Ingeniería, núm. 30 (2026). pp. 30-55
https://doi.org/10.36561/ING.30.4
ISSN 2301-1092 ISSN (en línea) 2301-1106 Universidad de Montevideo, Uruguay
37
Likewise, for the rear quadrant:
󰇛󰇜
 󰇥󰇡
󰇛󰇜
󰇢󰇦 [2]
where, x, y, and z are the local spatial coordinates.
  [3]
where V is the Voltage (V), I is the current (A), and η is the thermal efficiency (%).
The product of the voltage (V), current (I), and thermal efficiency (η), is typically 80% for SMAW, which means that
power provided by the welding source is 80% converted to the thermal energy required for welding. ν is the welding
speed and t is the present time.
The and are the heat fraction parameters for the front and rear quadrants respectively, and their sum is equal to
two. The recommended values stated by Goldak et al. (1984) are = 0.6 and = 1.4.
The thermal analysis of the 3D model involves the most important factor known to be the conservation of energy.
The governing equation related to transient heat transfer analysis in welding is denoted by (Equation [3]) [47].

 󰇛󰇜 󰇛󰇜󰇛󰇜 [4]
where, is the density of materials (
), c is the specific heat capacity, T is the current temperature, is the flux
vector, Q is the internal rate of heat generation, x, y, and z are the coordinates in the reference system, and t is time.
It is assumed that there will be radiation losses from the outer surface of the plates by both, convection, and
radiation. The heat losses will be prominent around and in the weldment via radiation whereas the area away from
the weld zone will experience heat loss through convection [48], [49]. Hence, a combined heat transfer coefficient is
used and computed from (Equation [5]) [50].
󰇛󰇛󰇜󰇛󰇜󰇜
󰇛󰇜 [5]
where,
is the combined heat transfer coefficient,  is the emissivity  the Stefan Boltzmann constant,  is
the ambient temperature, and is the convective heat transfer coefficient.
The parameters in the 3D double ellipsoidal model are given in the following Table III and the welding parameters in
Table IV. Goldak’s double ellipsoidal 3D heat source model is validated with the experimental results obtained by
Christensen et al [50].
Parameters
Value
Length of the front ellipsoid

12.9 mm
Length of the rear ellipsoid

10.3mm
Depth of penetration
b
3 mm
Width of heat source
a
8 mm
Front heat fraction
0.6
Rear heat fraction
1.4
Table III. Double ellipsoidal heat source parameters [51].
S. F. Haider, S. A. Khan, A. Shah, M. N. Bashir, A. Mansoor, A. Hussain, M. M. Ali, S. Nisar
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Welding Parameters
Values
Arc Voltage
V
22 V
24 V
26 V
Current
I
120 A
140 A
160 A
Welding Speed
vel
3 mm/s
5 mm/s
7 mm/s
Heat Source Efficiency
η
80%
Table IV. Welding Parameters for SMAW [39].
2.3 Design of Experiments (DOE). - The excessive current and voltage during the welding process may induce stresses
and distortion in the welding geometry along with other defects. Also, the lower current and voltage settings may result
in incomplete joint penetration and more spatter. Moreover, slow welding speed leads to concentrated heat input at a
particular weld location which causes distortion. On the other hand, the fast-welding speed leads to incomplete weld
penetration but less distortion. These effects cause weak welding strength and poor weld quality.
To cater to this issue, the process parameters require optimization either via several experiments or through a parametric
numerical simulation. So, the simulation tool for analysis and optimization of SMAW process parameters is to be used.
Therefore, a 3D simulation of weld geometry with modules coupled (Heat transfer with Solid Mechanics) in COMSOL
Multiphysics 5.5 simulation software is built for the present study.
The Box-Behnken Design (BBD) is a form of response surface methodology (RSM) that requires at least three levels
to run a single experiment. In this study, the three-level-three-factor BBD technique was applied to obtain the best
combination of welding variables for the sound quality of the weld [52], [53], [54], [55], [56]. Table V represents the
chosen welding variables along with their levels.
Order No.
LEVELS USING BBD
ACTUAL VALUES
V
I
vel
V
I
vel
1
-1
-1
0
22
120
0.005
2
-1
1
0
22
160
0.005
3
1
-1
0
26
120
0.005
4
1
1
0
26
160
0.005
5
-1
0
-1
22
140
0.003
6
-1
0
1
22
140
0.007
7
1
0
-1
26
140
0.003
8
1
0
1
26
140
0.007
9
0
-1
-1
24
120
0.003
10
0
-1
1
24
120
0.007
11
0
1
-1
24
160
0.003
12
0
1
1
24
160
0.007
13
0
0
0
24
140
0.005
14
0
0
0
24
140
0.005
15
0
0
0
24
140
0.005
Table V. Assigning Levels to the Process Parameters.
S. F. Haider, S. A. Khan, A. Shah, M. N. Bashir, A. Mansoor, A. Hussain, M. M. Ali, S. Nisar
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There are three levels i.e., -1, 0, and 1 for each parameter which corresponds to the lowest level, central level, and the
highest level of parameter values. Table V shows 15 different combinations of input process parameters with the levels
assigned and the actual values of the input parameters.
2.4 Simulation Procedure. - The 3D graphical model of the welded joint was developed in SOLIDWORKS 2016 and
imported into COMSOL Multiphysics 5.5 for the thermo-mechanical simulation of the SMAW process. The geometry
consists of two steel plates (S355J2+N and ASTM A572 Gr.50) and a central weld region configured as a Single-V
groove butt joint, following ISO-9692 recommendations for joint preparation [43].
The Heat Transfer in Solids and Solid Mechanics physics interfaces were applied in a coupled manner to capture both
the transient thermal response and the resulting elastic deformation. Goldak’s double-ellipsoidal heat source
formulation was implemented according to the procedure described in [4446], and the associated welding parameters
are summarized in Table VI. The initial temperature was set at 25 °C, and heat losses from external surfaces were
treated using convection and radiation boundary conditions based on the methodology described in [4850]. The total
heat input was calculated using the arc efficiency for SMAW reported in [51].
Parameter
Value
Description
x0
-0.10 m
Heat source center x-coordinate
y0
0 m
Heat source center y-coordinate
z0
-0.002 m
Heat source center z-coordinate
vel
0.003 m/s
Welding speed
V
22 V
Welding voltage
I
120 A
Welding current
u
0.8
Weld efficiency
af
0.0129 m
Length of front ellipsoidal
ar
0.0103 m
Length of rear ellipsoidal
b
0.003 m
Depth of penetration
c
0.005 m
Width of heat source
Ff
0.6
Heat fraction (front)
Fr
1.4
Heat fraction (rear)
cf
0.0129 m
Front length of the weld pool
cr
0.0103 m
Rear length of the weld pool
Q
3200
Heat input
S. F. Haider, S. A. Khan, A. Shah, M. N. Bashir, A. Mansoor, A. Hussain, M. M. Ali, S. Nisar
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a
0.008 m
Weld width/2
q01
1.1574 x 
Power density Distribution for the front part
q02
3.3823 x 
Power density distribution for the rear part
p
1.0133 x  Pa
Pressure
Table VI. Defining the parameters for the 3D geometry.
The resulting transient temperature field was then used as a thermal load in the structural analysis. All materials were
modelled as linear elastic, consistent with the simplified thermo-elastic welding models commonly reported in earlier
studies [57], [58]. Temperature-dependent mechanical properties, plasticity, creep, and phase transformation effects
were not included, and therefore the mechanical results represent elastic strain-based indicators of deformation rather
than true physical residual stress magnitudes. Accordingly, the von Mises stress values are interpreted only for
comparative analysis between welding conditions, not as actual residual stresses.
A free boundary condition was applied to allow unconstrained deformation of the plates. No external clamps or fixtures
were used. The absence of mechanical constraints allows free distortion and therefore represents an upper-bound
estimate of deformation, while constrained welding conditions would be expected to reduce out-of-plane displacement
but increase residual stresses.
The simulation was run as a time-dependent study from 0 to 67 s, corresponding to the weld-travel time at 0.003 m/s,
while higher speeds (0.005 and 0.007 m/s) reduced the welding duration to approximately 40 s.
The mesh was generated using physics-controlled tetrahedral elements, with refinement along the weld line to capture
steep thermal gradients. This meshing strategy follows recommendations in prior finite element welding simulations
[36], [37], [40]. Figure 3 shows the final meshed geometry.
Figure III. Meshing strategy employed for the SMAW numerical model
In this study, the simulation time range was set from 0 to 67 s with a time step of 0.05 s. At a welding speed of 0.003
m/s, the 200 mm weld length requires approximately 67 s for completion in a single pass. At higher speeds of 0.005
m/s and 0.007 m/s, the same weld length is completed in approximately 40 s.
S. F. Haider, S. A. Khan, A. Shah, M. N. Bashir, A. Mansoor, A. Hussain, M. M. Ali, S. Nisar
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2.5 Temperature Profiles. - Figure 4 illustrates the evolution of the temperature field as the Goldak double-ellipsoidal
heat source moves along the weld line in the x-direction. Welding begins from the left-hand side of the joint, and the
transient temperature contours at four representative times (t = 15 s, 25 s, 30 s, and 35 s) are shown in Figures 4(ad).
The highest temperatures occur in the weld pool and the immediate heat-affected zone, while temperatures decrease
rapidly away from the heat source due to conduction and surface heat losses.
Figure IV. Goldak double-ellipsoidal heat source representation used to model arc heat input in the SMAW process
(a) t = 15s, (b) t = 25s, (c) t = 30s, (d) t =35s.
Figures 5(a) and 5(b) present the temperature distribution along the depth (z-axis) and the transverse direction (y-axis),
respectively. As expected, the temperature decreases with depth below the weld centerline and laterally across the plate
thickness. Once the local temperature exceeds approximately 1425 °C, melting initiates, and the weld metal begins to
form the fusion bond at the joint interface.
Figure V. Transient temperature distribution. (a)Temperature vs Z-coordinate, and (b) Temperature vs Y-
coordinates.
M.P = 1425° C
(
(
b
S. F. Haider, S. A. Khan, A. Shah, M. N. Bashir, A. Mansoor, A. Hussain, M. M. Ali, S. Nisar
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2.6 Structural Stresses and Deformation. - Figures 6(a) and 6(b) present the elastic von Mises stress indicator
obtained from the thermo-elastic structural model. As noted earlier, the mechanical analysis was performed using
linear-elastic material behaviour; therefore, the reported von Mises values represent qualitative elastic stress indicators
rather than physical residual stress magnitudes. These indicators highlight regions where the thermal cycle generates
high elastic strain and provide insight into the relative stress distribution during and immediately after welding.
Elevated elastic stress indicators appear near the weld centerline, where the material experiences the largest thermal
gradients and volumetric expansion. Away from the weld pool, the indicator decreases rapidly as the temperature field
becomes more uniform. Along the transverse (y-axis) direction, the maximum indicator occurs near the weld centerline,
while along the longitudinal (x-axis) direction the distribution varies with the non-uniform heat input and the
progression of the heat source. These trends are shown in Figures 7(a) and 7(b).
The deformation field resulting from thermal expansion and subsequent cooling is shown in Figures 8(ac). The
predicted distortion reflects the accumulated elastic strains, with maximum displacement occurring near the edges and
corners of the welded plates. The Z-component displacement illustrates upward bending near the weld region, which
is consistent with typical distortion behavior in butt-welded joints subjected to steep temperature gradients.
These qualitative results demonstrate how variations in heat input influence the overall deformation pattern. While
quantitative residual stress predictions require elasticplastic, temperature-dependent modelling, the present thermo-
elastic simulation provides useful comparative insight into the effect of welding parameters on the distribution and
magnitude of elastic strain and distortion.
Figure VI. Elastic von Mises stress indicator distribution obtained from the linear thermo-elastic structural model at
V = 24 V, I = 150 A, and welding speed = 0.004 m/s at t = 14 s: (a) yz plane section through the weld centerline;
(b) isometric view. The plotted values represent qualitative elastic stress indicators and do not correspond to true
residual stresses.
S. F. Haider, S. A. Khan, A. Shah, M. N. Bashir, A. Mansoor, A. Hussain, M. M. Ali, S. Nisar
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Figure VII. Distribution of the elastic von Mises indicator along (a) the longitudinal (x) direction and (b) the
transverse (y) direction relative to the weld centerline.
Figure VIII. Predicted displacement field from transient thermal loading: (a) global displacement magnitude, (b)
isometric view of deformation, (c) Z-component displacement illustrating out-of-plane distortion after cooling.
S. F. Haider, S. A. Khan, A. Shah, M. N. Bashir, A. Mansoor, A. Hussain, M. M. Ali, S. Nisar
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3. Results and Discussion. -
3.1 Design of Experiments and Statistical Modelling. - A BoxBehnken Design (BBD) with three factors and three
levels was employed to evaluate the influence of welding voltage, current, and welding speed on the thermo
mechanical responses of the welded joint. Multiple regression analysis was conducted following the procedures
described in [59], using the response data summarized in Table VII.
Because the structural model was linear-elastic, the von Mises output (Res_Str) represents an elastic stress indicator
rather than a physical residual stress. Therefore, quantitative regression and ANOVA were performed only for the
physically meaningful responses, namely the Z-displacement (Td) and the maximum temperature (T_max). The elastic
stress indicator (Res_Str) is retained in Table VII for qualitative comparison only and was not used to develop empirical
equations.
A general parametric relationship of the form presented below was fitted to the log-transformed data for Td and
T_max:.   [6]
where corresponds to log(Td) or log(T_max), X₁ = log(V), X₂ = log(I), and X₃ = log(vel).
A log-linear model of the form shown in Equation [6] was fitted to log-transformed responses, where the predictors
correspond to log(V), log(I), and log(vel). The regression coefficients were estimated using Microsoft Excel based on
the approach in [59].
Order No.
Levels Defined
Actual Values
Response Parameters
V
I
vel
V
I
vel
Res_Str
Td
T_max
(GPa)
(mm)
(°C)
1
-1
-1
0
22
120
0.005
3.581E+09
0.0679
1090.2
2
-1
1
0
22
160
0.005
4.638E+09
0.0939
1585
3
1
-1
0
26
120
0.005
3.122E+09
0.0805
1334.9
4
1
1
0
26
160
0.005
1.468E+09
0.0486
2506.5
5
-1
0
-1
22
140
0.003
1.722E+09
0.062
2538.8
6
-1
0
1
22
140
0.007
1.13E+09
0.0573
1924.7
7
1
0
-1
26
140
0.003
1.679E+09
0.0555
3044.9
8
1
0
1
26
140
0.007
5.578E+09
0.0942
1500.8
9
0
-1
-1
24
120
0.003
2.32E+09
0.07
1994.7
10
0
-1
1
24
120
0.007
3.094E+09
0.0738
1103.7
11
0
1
-1
24
160
0.003
2.702E+09
0.0544
3494.1
12
0
1
1
24
160
0.007
3.315E+09
0.0992
1618.6
13
0
0
0
24
140
0.005
5.912E+09
0.0885
1488.2
14
0
0
0
24
140
0.005
5.912E+09
0.0884
1483.1
15
0
0
0
24
140
0.005
5.912E+09
0.0894
1489.3
Table VII. BBD Design and Output response values of Residual Stress (Res_Str), Displacement (Td), and Maximum
Temperature (T_max)
S. F. Haider, S. A. Khan, A. Shah, M. N. Bashir, A. Mansoor, A. Hussain, M. M. Ali, S. Nisar
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Figure IX. Scatter plots comparing actual and predicted responses for (a) distortion (Td) and (b) maximum
temperature (T_max) based on log-linear regression models. The elastic stress indicator (Res_Str) is shown for
completeness but was not used for regression analysis.
The regression results are summarized in Table VIII. The scatter plots of actual versus predicted values for Td and
T_max are shown in Figures 9(ab), demonstrating reasonable agreement between the predicted and observed
responses, consistent with the use of log-transformed linear models [6164].
Source
log Res_Str
log Td
log T_max
F-value
p-value
F-value
p-value
F-value
p-value
Model
0.3441
0.0535
1.1130
0.9738
13.0007
0.0477
log V
-
0.8352
-
0.9072
-
0.2897
log I
-
0.8879
-
0.8514
-
0.0031
log vel
-
0.3467
-
0.0971
-
0.0005
R-sq
0.0858
0.2328
0.7800
R-sq (adj)
-0.1635
0.0236
0.7200
Table VIII. ANOVA results for log Res_Str, log Td, and log T_max
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The low value for Td indicates that a first-order log-linear model is insufficient to fully capture deformation
behaviour, which is influenced by geometric stiffness and boundary effects beyond primary process parameters. The
ANOVA results indicate that welding current exhibits the strongest statistical influence on T_max, as evidenced by
the lowest p-value, followed by welding speed and voltage. For Td, the p-values are comparatively higher, indicating
weaker explanatory power. This aligns with the sensitivity considerations described widely in welding DOE literature
[6569], in which T_max is generally more sensitive to heat-input variations than displacement.
Because Res_Str is an elastic indicator and not a physical residual stress, no empirical equation or sensitivity expression
is provided for that quantity.
A formal optimization or multi-objective decision-making procedure was not performed; therefore, the results are
interpreted as parametric trends rather than optimized welding conditions.
3.2 Thermal Response. - Figures 10(a) and 10(b) illustrate the maximum temperature variation along the weld line (x-
axis) and through the depth (z-axis). The temperature rises rapidly once the arc initiates, reaches a peak sufficient for melting
and fusion, and fluctuates slightly along the x-direction due to the evolving heat-sink effect of the surrounding base metal.
Along the z-axis, the temperature decreases with depth as heat is conducted away from the active fusion zone. These thermal
cycles govern melting, fusion, and the subsequent development of distortion.
Figure X. Variation of maximum temperature (T_max) along (a) the weld line (x-axis) and (b) through the plate
thickness (z-axis) during welding.
S. F. Haider, S. A. Khan, A. Shah, M. N. Bashir, A. Mansoor, A. Hussain, M. M. Ali, S. Nisar
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The thermal expansion and contraction associated with the heating and cooling cycle induce elastic strain fields, which
are represented by the elastic von Mises indicator (Res_Str). As discussed earlier, this quantity does not represent true
residual stress but provides a qualitative map of regions experiencing higher thermo-elastic loading during welding.
Distortion (Td) reflects the cumulative effect of these elastic strains and the steep temperature gradients in the joint.
Minimizing weld volume, optimizing heat input, and controlling inter-pass timing are common methods for reducing
distortion in welded joints, as reported in previous studies [70], [71]. These general concepts are consistent with the
qualitative trends observed in the present thermo-elastic model.
3.3 Heat Source benchmarking. - The Goldak double-ellipsoidal volumetric heat source implemented in this study
was benchmarked by examining the thermal field behaviour, fusion-zone dimensions, and the temperature-time
response at points adjacent to the weld line. The objective was to ensure that the implemented heat input parameters
reproduced the characteristic features of SMAW thermal behaviour reported in the literature.
Figure IV shows the transient thermal distribution as the heat source travels along the weld line. The predicted peak
temperatures exceed the melting range of the steel (~14251500 °C), followed by rapid cooling once the heat source
moves forward. This behaviour is consistent with established SMAW thermal cycles, where peak temperatures remain
concentrated in the fusion zone and decrease sharply within a few millimeters of the weld centreline [4446], [4850].
The predicted fusion-zone width and depth estimated from the isotherms near the melting temperature agree in
magnitude with typical SMAW fusion zones reported for similar heat inputs and plate thicknesses in earlier numerical
and experimental studies [36], [40], [57]. The predicted fusion zone depth of ~3 mm falls within the 2.53.5 mm range
reported by Goldak et al.[50] for comparable SMAW heat inputs.Although the present model does not include phase
transformations, the overall size and shape of the molten region fall within expected ranges for comparable voltage,
current, and travel speed combinations.
The temperaturetime history extracted along the weld line (Figure 11(a)) demonstrates the expected progression from
rapid heating to steep cooling. The temperature fluctuations along the x-direction, including the lower temperature
observed immediately at arc initiation and the slight peak towards the end of the weld, are characteristic of Goldak-
type heat input profiles and reflect the evolving heat-sink conditions of the surrounding base metal. The temperature
variation through the depth (Figure 11(b)) shows decreasing temperature with increasing depth, as documented in
earlier SMAW simulations [47], [48].
Overall, the shape of the fusion zone, the magnitude and gradient of peak temperatures, and the transient behaviour of
the temperature field confirm that the implemented Goldak heat source is physically consistent and aligns well with
previously published numerical welding models.
3.4 Discussion. - The thermomechanical simulations performed in this study provide a clear understanding of how
SMAW process parameters influence the thermal field, elastic strain distribution, and deformation in a Single-V butt
joint configuration. The predicted temperature distribution is consistent with the behaviour expected from a Goldak
double-ellipsoidal heat source, where the highest temperatures occur near the weld pool and rapidly decrease away
from the fusion zone due to conduction and surface heat losses. The thermal gradients observed in Figures 4 and 5
follow the characteristic pattern reported in earlier numerical welding studies [4446], [4850], confirming correct
representation of heat input and boundary conditions.
The thermal results further show that welding current and welding speed significantly influence peak temperature
levels (T_max). Higher current increases heat input per unit length, resulting in a wider and deeper fusion zone,
whereas higher speed reduces the time available for heat accumulation, thereby decreasing T_max. These parametric
trends are consistent with SMAW physics and with previous findings in the literature [36], [40], [57]. The temperature
evolution along the weld line and through the depth (Figure 11) confirms that the weld pool experiences a rapid heating
phase, followed by accelerated cooling once the heat source moves forward. This behaviour governs the molten pool
development and the subsequent formation of the fusion zone.
S. F. Haider, S. A. Khan, A. Shah, M. N. Bashir, A. Mansoor, A. Hussain, M. M. Ali, S. Nisar
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The elastic von Mises indicator (Res_Str) provides qualitative insight into regions experiencing high thermo-elastic
loading during and immediately after welding. As expected, the highest elastic indicator values appear near the weld
centreline, where steep thermal gradients induce differential expansion. Although these values do not represent true
residual stresses due to the absence of plasticity in the structural model, the spatial trends in Figures 6 and 7 help
identify zones with the greatest deformation potential. Similar qualitative stressdistribution patterns have been
reported in simplified thermo-elastic welding simulations [57], [58].
The deformation results reveal that the dominant distortion mode is out-of-plane bending (Z-displacement), with peak
deflection occurring near the plate edges and corners (Figures 8(ac)). This is consistent with classical distortion
mechanisms associated with butt welding, where asymmetric heating causes upward bending due to non-uniform
expansion and contraction. The magnitude and distribution of Td are strongly influenced by heat input, aligning with
the behaviour noted in prior experimental and numerical work [6569].
The DOE and regression analysis provide further insight into parameter influence. The ANOVA results (Table VIII)
show that welding current exerts the strongest statistical effect on T_max, followed by welding speed, while Td exhibits
comparatively weak sensitivity to all three parameters. This behaviour reflects the dual dependence of distortion on
both thermal gradients and the structural stiffness of the plates. The relatively low values for Td also indicate that
deformation is influenced by geometric effects beyond the primary welding parameters, a trend also observed in earlier
welding DOEs [6264].
Although direct experimental validation for the S355J2+N / ASTM A572 Gr.50 joint was not available, the simulated
trends, namely the increase of peak temperature with welding current and its reduction with increasing welding speed,
are consistent with experimental and numerical observations reported for comparable arc-welded structural steels in
the literature [21, 22, 29]. Furthermore, the predicted distortion magnitudes fall within the ranges reported for butt-
welded steel plates subjected to similar heat inputs and boundary conditions [2426].
Overall, the present simulation framework successfully captures the key qualitative relationships between welding
parameters, thermal fields, and deformation. While the thermo-elastic model does not produce quantitative residual
stress values, it provides reliable comparative trends that can guide parameter selection for reducing distortion.
Incorporating temperature-dependent elastoplastic properties and phase transformation effects in future work will
enable accurate prediction of residual stress magnitudes and allow for full validation against experimental data.
3.5 Significance of the Study. - This study provides an integrated thermomechanical and design-of-experiments
assessment of the SMAW process for a Single-V butt joint of S355J2+N and ASTM A572 Gr.50 steels. By combining
a transient Goldak-type heat source model with thermo-elastic structural analysis and a BoxBehnken design, the work
establishes a coherent framework for understanding how voltage, current, and welding speed influence weld-pool
thermal cycles and distortion. The results clarify the dominant role of welding current in controlling peak temperatures
and demonstrate how increases in welding speed can effectively reduce thermal accumulation and limit out-of-plane
deformation.
Although the structural model is elastic and therefore does not predict true residual stress magnitudes, the elastic von
Mises indicator provides valuable qualitative insight into regions experiencing elevated thermo-elastic loading. This
enables identification of distortion-prone zones and supports the interpretation of deformation mechanisms without
requiring a full elastoplastic formulation.
The combined simulationDOE approach offers a practical methodology for parameter screening in welded structures
where distortion control is critical. The insights derived here can guide the selection of welding parameters for reducing
deformation in industrial fabrication settings. Moreover, the modelling structure developed in this work provides a
foundation for future enhancements involving temperature-dependent elastoplastic laws, phase-transformation effects,
and experimental validation. These extensions will further strengthen the predictive capability of numerical welding
simulations and contribute to optimized process planning in structural steel applications.
S. F. Haider, S. A. Khan, A. Shah, M. N. Bashir, A. Mansoor, A. Hussain, M. M. Ali, S. Nisar
Memoria Investigaciones en Ingeniería, núm. 30 (2026). pp. 30-55
https://doi.org/10.36561/ING.30.4
ISSN 2301-1092 ISSN (en línea) 2301-1106 Universidad de Montevideo, Uruguay
49
4. Conclusion and Future Work. - A three-dimensional transient thermo-mechanical finite element framework was
developed to investigate the influence of SMAW process parameters on the thermal and deformation behavior of
dissimilar S355J2+N and ASTM A572 Grade 50 steel plates. Based on the numerical simulations and parametric
analysis, the following conclusions can be drawn:
1. Welding current is the dominant parameter governing peak temperature, producing a strong increase in
maximum thermal response with increasing current, whereas travel speed significantly moderates thermal
gradients by controlling heat input per unit length.
2. Travel speed exerts the strongest influence on out-of-plane distortion, indicating its critical role in deformation
control during SMAW of structural steel joints. Voltage shows a secondary effect on both thermal distribution
and deformation behavior.
3. Elastic stress fields obtained from the linear thermo-elastic analysis reveal spatial stress localization
associated with thermal gradients; however, due to the absence of plasticity, stress relaxation, and
temperature-dependent material properties, these results are interpreted solely as qualitative elastic stress
indicators rather than physically realistic residual stresses.
4. Regression and ANOVA analyses support the qualitative identification of dominant parameters for peak
temperature and distortion; nevertheless, low coefficients of determination for certain responses indicate the
limitations of first-order models and restrict their use to trend interpretation rather than prediction or
optimization.
5. Benchmark comparisons with published experimental and numerical studies on comparable structural steels
demonstrate consistency in thermal and deformation trends, supporting the credibility of the numerical
framework within its stated scope.
The primary contribution of this work lies in providing a transparent thermo-elastic FEM and design-of-experiments
based sensitivity assessment for a dissimilar structural steel combination not previously reported in SMAW numerical
studies. The limitations associated with the material model and the absence of direct experimental validation are
explicitly acknowledged. Future work will focus on incorporating temperature-dependent material behavior, plasticity,
and experimental measurements to enable physically realistic residual stress prediction and quantitative model
validation.
Future research will extend the present numerical framework by incorporating temperature-dependent thermo-physical
and mechanical material properties, as well as elasticplastic constitutive behavior, to enable physically realistic
prediction of residual stresses and permanent deformation. The inclusion of phase transformation effects and stress
relaxation mechanisms will further improve the fidelity of the mechanical response during heating and cooling cycles.
Experimental measurements of temperature histories, fusion zone geometry, and distortion for the S355J2+N / ASTM
A572 Gr.50 joint will be pursued to provide direct quantitative validation of the numerical model. In addition, refined
response surface models incorporating higher-order and interaction terms, combined with formal multi-response
optimization techniques, will be employed to support predictive parameter selection and process optimization. These
extensions will allow the framework developed in the present study to evolve from qualitative parameter screening
toward quantitatively validated welding process design.
Declaration Conflict of Interest. - The authors of this research announce that they have no known contending
monetary interests or individual connections that may have impacted the work detailed in this paper.
Data and Code Availability. - Data and code shall be made available upon request to the corresponding author.
S. F. Haider, S. A. Khan, A. Shah, M. N. Bashir, A. Mansoor, A. Hussain, M. M. Ali, S. Nisar
Memoria Investigaciones en Ingeniería, núm. 30 (2026). pp. 30-55
https://doi.org/10.36561/ING.30.4
ISSN 2301-1092 ISSN (en línea) 2301-1106 Universidad de Montevideo, Uruguay
50
Nomenclature.
SMAW
Shielded Metal Arc Welding
FEM
Finite Element Method
HAZ
Heat Affected Zone
C
Carbon
Si
Silicon
Mn
Manganese
vel
Welding Speed
V
Voltage
I
Current
Density of materials
c
Specific heat capacity
T
Present temperature
Flux vector
Q
Internal rate of heat generation
x, y, z
Coordinates in the reference system
t
Time
Combined heat transfer coefficient

Emissivity

Stefan Boltzmann Constant

Ambient temperature

Convective heat transfer
Coefficient.
η
Thermal Efficiency

Length of the front ellipsoid
GMAW
Gas Metal Arc Welding
BBD
Box-Behnken Design
RSM
Response Surface Methodology

Length of the rear ellipsoid
a
Width of heat source
b
Depth of Penetration
Front heat fraction
MS
Mild Steel
Rear heat fraction
HB
Hardness Brinell
PWHT
Post-Weld Heat Treatment
DCEN
Direct Current Electrode Negative
DCEP
Direct Current Electrode Positive
AISI
American Iron and Steel Institute
ASTM
American Society for Testing and Materials
UTS
Ultimate Tensile Strength
EL%
Percentage Elongation
TIG
Tungsten Inert Gas
GTAW
Gas Tungsten Arc Welding
LPG
Liquefied Petroleum Gas
G
Groove
F
Fillet
SS
Stainless Steel
S355
Structural Steel with a minimum yield
strength of minimum 355 MP
S. F. Haider, S. A. Khan, A. Shah, M. N. Bashir, A. Mansoor, A. Hussain, M. M. Ali, S. Nisar
Memoria Investigaciones en Ingeniería, núm. 30 (2026). pp. 30-55
https://doi.org/10.36561/ING.30.4
ISSN 2301-1092 ISSN (en línea) 2301-1106 Universidad de Montevideo, Uruguay
51
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Memoria Investigaciones en Ingeniería, núm. 30 (2026). pp. 30-55
https://doi.org/10.36561/ING.30.4
ISSN 2301-1092 ISSN (en línea) 2301-1106 Universidad de Montevideo, Uruguay
55
Author contribution:
1. Conception and design of the study
2. Data acquisition
3. Data analysis
4. Discussion of the results
5. Writing of the manuscript
6. Approval of the last version of the manuscript
SFH has contributed to: 1, 2, 3, 4, 5 and 6.
SAK has contributed to: 1, 2, 3, 4, 5 and 6.
AS has contributed to: 1, 2, 3, 4, 5 and 6.
MNB has contributed to: 1, 2, 3, 4, 5 and 6.
AM has contributed to: 1, 2, 3, 4, 5 and 6.
AN has contributed to: 1, 2, 3, 4, 5 and 6.
MMA has contributed to: 1, 2, 3, 4, 5 and 6.
SN has contributed to: 1, 2, 3, 4, 5 and 6.
Acceptance Note: This article was approved by the journal editors Dr. Rafael Sotelo and Mag. Ing. Fernando A.
Hernández Gobertti.