# Multiattribute Assessment of Consumables for TIG Welding of Aluminum Alloys

Authors: P. K. Baghel; D. S. Nagesh
Journal: International Journal of Manufacturing Engineering
 (2016)

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## Abstract

Consumable materials for welding processes such as filler alloy, electrode, and shielding gas have major implications in welding technology. Selecting the appropriate set of consumable materials for welding aluminum alloys from various available alternates gives rise to a significant decision making problem. This study proposes a strategic justification tool based on integrated analytical hierarchy process, technique for order preference by similarity to ideal solution (AHP-TOPSIS), to screen and select the best possible combination of filler alloy, electrode, and shielding gas for TIG welding. Based on qualitative analysis of available alternates, ER5356 filler alloys and 0.8% zirconiated electrode are selected as suitable consumable in combination with pure argon as shielding gas. The proposed result is experimentally validated using mechanical property testing.


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## Body

## 1. Introduction

Dissimilar aluminum alloys combinations are widely used in aerospace and automobile applications such as inner body panel, heat shields, structural components, ladders, and space frames [1]. Several welding processes such as friction stir welding (FSW) and laser welding are gaining popularity for welding aluminum but TIG welding is still most widely used process for joining aluminum because of its heat control ability (narrow heat affected zone) and eco-friendly nature (no spatter and smoke). Although friction stir welding has several advantages like no voids and cracking, no distortion of workpiece, no need of filler material, no shielding gas required, clean and environment friendly process because there are no harmful effects like arc formation, radiation, release of toxic gas, and so forth, however as compared to TIG welding process some disadvantages of the friction stir welding process have been identified as well such that exit hole is left when the tool is withdrawn. This limitation is serious when pressure vessels and cargo oil tanks are manufactured. Heavy-duty clamping is required to hold the plates to combat large downward force. In addition to this it is less flexible that is difficult to weld when thickness varies.The ideal weld joint should have tensile strength close to base metal and must be free from hot cracks and residual stress. Consumable materials, namely, filler alloy, electrode, and shielding gas, play a vital role in deciding the manufacturing quality and cost of weld joint [2].When multiple choices are present, choosing the optimum material of desired properties from large number of available materials is a tedious task. It is essential to base the final decision using well-structured selection methodology in consideration with all possible relevant attributes or properties. Multiattribute decision making (MADM) models are generally used to provide an encompassing analysis of all involved multiple attributes.In an unstructured decision problem in welding processes, such models have recently been used by many researchers. Khorshidi et al. [3] used TOPSIS for selecting the optimal refinement condition to achieve maximum tensile property in Al-15% Mg2Si composite whereas Mirhedayatian et al. [4] employed TOPSIS approach and integrated fuzzy data envelopment analysis in welding process selection for repairing nodular cast iron engine block.The selection of consumable materials is of prime importance to accomplish the joint of desired specifications; however there are not enough investigations in this direction. Therefore there is a need for an extensive selection framework before undertaking the manufacturing process.In present research, technique for order preference by similarity to ideal solution (TOPSIS) integrated with analytical hierarchy process (AHP) is employed to select an optimal combination of consumable materials for welding dissimilar aluminum alloys.


## 2. Materials and Methodology

Consumables in welding processes comprise filler alloy, electrode material, and shielding gas. The filler alloy determines the transverse and longitudinal strength of the weld joint. Therefore the filler material should have attributes like high tensile properties, impact toughness, and low cost. There are mainly five filler alloys that are used and listed in Table1.Table 1
List of attributes and alternates for filler alloy [1].
Properties ER5356 ER5556 ER5183 ER5654 ER5554 (1) Yield strength (MPa) 240 158.579 275 220.63 124.10 (2) Tensile strength (MPa) 268.89 317.15 296.47 227.52 186 (3) Elongation 2% 17 14 17 17 8 (4) Brinell hardness (HB) 105 65 99 83 39 (@load 500 Kg: thickness 10:ohm) (5) Cost ($) 13.5 16 15.5 17.2 13 (6) Longitudinal shear strength (MPa) 117.21 137.89 127.55 82.73 79.289 (7) Transverse shear strength (MPa) 179.26 206.84 193.05 124.10 103.42 (8) Impact strength (J) 18.2 15.7 16 13 10Table2 presents the alternates and attributes of electrode used in pulse TIG welding of aluminum alloys. Tungsten electrode used in TIG welding is a consumable. It merely serves as the terminal for the electric arc which produces the heat needed to join the base metal being welded. The shape of the tungsten electrode tip is an important process variable in GTA welding. Tungsten electrode geometry has an effect on the arc shape (thereby affecting the weld bead size and shape), the weld penetration, and point longevity of the electrode. In addition to the arc shape, different tungsten materials pose different characteristics which influence arc start ability, electrode life, and contamination resistance.Table 2
List of attributes and alternates for electrode [2].
Properties Pure tungsten 2% thoriated 2% ceriated 1.5% lanthanated 0.8% zirconiated (1) Electrode oxide 0.01 2.6 3.2 2.5 0.3 work function (eV) (2) Density (g/cm3) 19.25 11.72 6.65 5.7 6.49 (3) Volume % of 2% 6 3.8 5.2 5.7 6.9 weight of electrode (4) Melting point (°C) 3410 1750 795 826 1852 (5) Electron negativity 1.7 1.3 1.0 1.1 1.2 (according to pauling) (6) Cost ($) 23.99 14.99 18.4 23.99 20.3 (7) Particle size (Nm) 30 50 40 20 30Selection of right shielding gas composition significantly affects metallurgical structure, properties, soundness, and heat treated response of weld. The desired characteristics with suitable alternates are listed in Table3.Table 3
List of attributes and alternates for shielding gas [7, 8].
Properties Pure argon Pure helium 25% argon + 75% helium 75% argon + 25% helium 50% argon + 50% helium (1) Thermal conductivity 0.016 0.1513 0.1174 0.0498 0.0836 W/mK at (1.013 bar at 0°C) (2) Gas density (lb/wft) at 0°C, 1 atm 0.1114 0.0111 0.0361 0.0863 0.0612 (3) Specific gravity (g/cm3) air = l 1.38 0.1368 0.4476 1.0692 0.7584 (4) Ionization potential (eV) 15.7 24.5 22.3 17.9 20.1 (5) Cost (per 100 g) ($) 0.5 5.2 4.025 1.675 4.15 (6) Specific heat capacity at 0.520 5.19 4.0225 1.6875 2.855 kJ/Kg·KCp (1.013 bar and 25°C)TOPSIS method is employed to evaluate and find the best suitable alternative in the present work. It was first proposed in 1981 [5].The methodology involves the evaluation of Euclidean distance from the positive and the negative ideal solution for the given alternate. The best possible alternative will be closest to the positive ideal solution and far away from negative ideal solution.TOPSIS is a suitable choice for material selection as it is a relatively more systematic process. It provides both qualitative and quantitative analysis of the available data. The TOPSIS method involves a tool for evaluation of weights of each attribute/criterion. In this study, this task is performed using AHP method. The relative weights hence generated are used in TOPSIS process to find the final priority ranking of available alternatives.It was developed by Satty [6] to handle complex problems based on multiple criteria. The flexibility and intuitiveness of AHP method provide edge over other methods. It facilitates group decision making by finding the geometric mean of the individual pairwise comparisons.Figure1 depicts (AHP-TOPSIS) MADM methodology for welding process consumables selection.Figure 1
Flow chart depicting integrated AHP-TOPSIS methodology for consumable materials selection.The AHP Method. To determine the relative importance of different attributes with respect to the objective the following steps are followed.The multiple pairwise comparisons are based on a standardized comparison scale of nine levels (Table4).Table 4
Nine-point intensity of importance scale.
Relative importance (aij) Description (i over j) 1 Equal importance 3 Moderate importance 5 Strong importance 7 Very strong importance 9 Absolute importance 2, 4, 6, 8 Intermediate valuesLetC={Cj∣j=1,2,…,n} be the set of criteria.The result of the pairwise comparison onn criteria can be summarized in an (n×n) evaluation matrix A. Every element aij(i,j=1,2,…,n) denotes the relative importance of factor i with respect to factor j. A criterion compared with itself is always assigned the value 1 so the main diagonal entries of the pairwise comparison matrix are all 1.Square matrixA containing every element aij is shown in(1)A=1a12⋯a1ma211⋯a2m⋮⋯⋮⋮am1am2⋯1,aij=1aji,aji≠0.(i)
The relative normalized weight (Wi) of each factor is evaluated by finding the geometric mean of ith row and normalizing the geometric means of rows in the comparison matrix(2)GMi=ai1×ai2×ai3×⋯×aij1/n,Wi=GMi∑j=1j=nGMi.Matrix X is obtained to denote an n-dimensional column vector. The sum of the weighted values is computed for the importance degrees of alternatives; then X=A∗W, where(3)W=W1,W2,W3,…,WnT,X=A∗W=1a12⋯a1na211⋯a2n⋮⋮⋯⋮an1an2⋯1W1W2⋮Wn=C1C2⋮Cn.(ii)
The consistency values (CV) are calculated for the cluster of alternatives represented by the vector(4)CVi=CiWi.(iii)
The largest eigenvalueλmax is obtained which is the mean of the consistency values.(iv)
The consistency index (CI) is calculated by(5)CI=λmax-nn-1.The AHP output quality is strictly related to the consistency of the pairwise comparison judgements.(vi)
The random index (RI) is obtained for the number of factors being used in decision making (Table 5).(vii)
The final consistency ratio (CR) is calculated as the ratio of the CI and CR(6)CR=CIRI.The acceptable upper limit for CR is 0.1. The evaluation process has to be repeated to improve the consistency, if the final consistency ratio exceeds this value. This consistency check is essential to establish the validity of the pairwise comparison matrix evaluation.Table 5
Random index (RI) values.
Criteria R I Criteria R I 3 0.52 7 1.35 4 0.89 8 1.40 5 1.11 9 1.45 6 1.25 10 1.49TOPSIS method consists of the following steps.Step 1 (construction of the normalized decision matrix).
For the Euclidean length of a vector, the elementrij of the normalized decision matrix R is evaluated using the following transformation:(7)rij=Xij∑i=1mXij2,j=1,2,…,n;i=1,2,…,m.Here, rij is the normalized preference measure of the ith alternative. “m” is the number of alternatives, and “n” is the number of criteria.Step 2 (construction of the weighted normalized decision matrix).
Multiply the columns of the normalized decision matrix with the set of weights obtained by AHP.W = ( w 1 , w 2 , w 3 , … , w n ) to obtain weighted normalized decision matrix:(8)V=RW=w1·r11w2·r12⋯wn·r1nw1·r21w2·r22⋯wn·r2n⋮⋮⋮w1·rm1w2·rm2⋯wn·rmn.Step 3 (determination of the ideal and negative ideal solutions).
The ideal solution and negative ideal solution value sets are determined, respectively, as follows:(9)V1+,V2+,…,Vn+=maxi⁡Vij∣J∈K,mini⁡Vij∣J∈K′∣i=1,2,…,m,V1-,V2-,…,Vn-=mini⁡Vij∣J∈K,maxi⁡Vij∣J∈K′∣i=1,2,…,m,where(10)K=j=1,2,3,…,n,jis  associated  with  benefit  criteria,K′=j=1,2,3,…,n,jis  associated  with  cost  criteria.Step 4 (measurement of separation distances from ideal and negative ideal solutions).
Euclidean distances for each alternative are, respectively, calculated as(11)Si+=∑j=1nVij-Vj+21/2;i=1,2,…,m,Si-=∑j=1nVij-Vj-21/2;i=1,2,…,m.Step 5 (calculation of the relative closeness to the ideal solution).
The relative closeness to the ideal solution can be defined as(12)Ci=Si-Si++Si-;i=1,2,…,m;0≤Ci≤1.The higher the closeness means the better the rank.Step 6 (ranking of the preference order).
The preference order is ranked on the basis of the order ofCi. Hence, the optimum alternative is the one which is nearer to the ideal solution and farther to the negative ideal solution.


## 3. Result and Discussion

### 3.1. Computational Results

The normalized decision matrix for filler alloy, electrode, and shielding gas is calculated using (7) as shown in matrices (13), (14), and (15), respectively,(13)0.53510.42620.50640.57400.39940.47020.48210.54010.31560.56320.41700.35530.47340.55310.55620.46590.59000.48840.50640.54120.45860.51160.51910.47480.45280.39180.50640.45380.50890.33180.33370.38580.24700.33030.23830.21320.38460.31800.27810.2967,(14)0.00210.76910.47810.77350.59270.52030.37800.54010.53830.46820.30280.39700.45330.32510.63000.46590.66250.26570.41430.18030.34870.39900.50400.47480.51760.22770.45420.18740.38350.52030.25200.38580.06210.25930.54980.42010.41840.44030.37800.2967,(15)0.07430.70420.70410.34520.07050.06270.70240.07020.06980.53870.70380.65250.54500.22820.22840.49030.54550.50500.23120.54550.54550.39360.22880.21020.38810.38690.38690.44200.38710.5207.These weights of all attributes of respective consumables are evaluated using AHP method and the results are presented in Table 6.Table 6
Weights of the attributes from AHP method.
Attributes Filler alloy weights Electrode weights Shielding gas weights A 1 0.0326 0.0311 0.0428 A 2 0.0235 0.0447 0.1006 A 3 0.0476 0.1586 0.1595 A 4 0.1059 0.1036 0.0640 A 5 0.3313 0.2399 0.2504 A 6 0.1572 0.3542 0.3824 A 7 0.2306 0.0675 A 8 0.0709A weighted normalized decision matrix for filler alloy, electrode, and shielding gas is presented in matrices (16)(16)0.01740.01000.02410.06080.13230.07390.11120.04270.01030.01320.01990.03760.15680.08690.12830.03680.01920.01150.02410.05730.15190.08040.11970.03750.01480.00920.02410.04810.16860.05220.07700.03050.00810.00780.01130.02260.12740.05000.06410.0234,0.00010.03440.07550.07970.14170.18420.02550.04270.01670.02090.04780.04090.10830.11510.04250.03680.02060.01190.06550.01860.08330.14130.03400.03750.01610.01020.07180.01930.09170.18420.01700.03050.00190.01160.08690.04330.10000.15580.02550.0234,0.00320.07080.11230.02210.01770.02400.03010.00710.01110.03450.17620.24950.02330.02300.03640.03140.13660.19310.00990.05490.08700.02520.05730.08040.01660.03890.06170.02830.09690.1991.


### 3.2. Ranking Results

The relative closeness to the ideal solution hence can be found using (12). The ranks are assigned based on their “C” values and are given in Table 7. The larger the value of closeness the better the rank.Table 7
TOPSIS analysis result.
Filler alloy Electrode Shielding gas Alternates C i Rank Alternates C i Rank Alternates C i Rank ER5356 (C1) 0.8358 1 Pure tungsten (C1) 0.4084 4 Pure argon (C1) 0.7149 1 ER5556 (C2) 0.6184 3 2% thoriated (C2) 0.5789 2 Pure helium (C2) 0.2850 4 ER5183 (C3) 0.7205 2 2% ceriated (C3) 0.4745 3 25% argon + 75% helium (C3) 0.3280 3 ER5654 (C4) 0.3142 5 1.5% lanthanated (C4) 0.2835 5 75% argon + 25% helium (C4) 0.6719 2 ER5554 (C5) 0.3516 4 0.8% zirconiated (C5) 0.5869 1 50% argon + 50% helium (C5) 0.2363 5It can be concluded from Table7, filler alloy, ER5356 has the highest ranking followed by ER5183 while ER5654 is the least ranked material. In arc electrode selection problem the optimum arc electrode is 0.8% zirconiated electrode which is the best alternate as it has slightly higher “C” value than 2% thoriated electrode. Shielding gas analysis results indicate pure argon as the optimum consumable component closely followed by Ar-He gas blend as second best alternative. The block diagram for material selection application has been shown in Figure 2.Figure 2
Block diagram for material selection application.


### 3.3. Welding Experimentation

The butt welding of aluminum alloy of 5083-O and 6061-T651 using pulse TIG welding (Triton 220 AC/DC) is performed to establish the applicability and validity of the selection model.The chemical composition of filler alloys used has been depicted in Table8.Table 8
Chemical composition of filler alloys used.
Composition Si Mg Fe Cu Mn Cr Zn Ti Al ER5356 0.23 5.0 0.40 0.05 0.12 0.9 0.10 0.13 Balance ER5556 0.25 5.1 0.40 0.10 0.75 0.13 0.25 0.13 Balance ER5183 0.40 4.8 0.40 0.10 0.75 0.15 0.25 0.15 Balance ER5654 0.22 3.5 0.23 0.05 0.01 0.25 0.20 0.10 Balance ER5554 0.25 2.7 0.40 0.10 0.75 0.13 0.25 0.13 BalanceExperimental validation has been conducted using highest ranking materials, namely, ER5356 as filler alloy, 0.8% zirconiated electrode, and pure argon shielding gas as shown in Figure3.Figure 3
Flow diagram depicting applications of 5083-O and 6061-T651.


#### 3.3.1. Radiography Examination

Welding was examined using radiography to check lack of penetration as shown in Figure4. No visual defects are observed in radiography film indicating proper fusion in weld joint leading to successful welding. 10 × 12 cm is the scale bar used.Figure 4
(a) Weld joint 5083-O + 6061 T-651. (b) Radiography.


#### 3.3.2. Microstructure Characterizations

Microstructural characterization is important since various characteristics of phase particles especially mechanical properties, corrosion resistance, are dependent on form of Mg2Si in which it exists in a particular material.Microstructural characterization uses optical microscope and SEM (scanning electron microscope) images (3700N Hitachi) to check grain refining and formation of brittle phase shown in Figure5.Figure 5
Microstructure (200x) and SEM (5μm) images of base metal, heat affected zone, and fusion zone at both sides.Microstructure shows three different regions, that is, base metal, heat affected zone, and fusion zone on either side of weld. Figure6 shows fusion zone (FZ) region, in which fine equiaxed grains of aluminum solid solution containing soluble phase consisting of Mg2Si particles show proper grain refinement. Hence improved weld quality is accomplished.Figure 6
SEM image of Mg2Si particle.


## 3.1. Computational Results

The normalized decision matrix for filler alloy, electrode, and shielding gas is calculated using (7) as shown in matrices (13), (14), and (15), respectively,(13)0.53510.42620.50640.57400.39940.47020.48210.54010.31560.56320.41700.35530.47340.55310.55620.46590.59000.48840.50640.54120.45860.51160.51910.47480.45280.39180.50640.45380.50890.33180.33370.38580.24700.33030.23830.21320.38460.31800.27810.2967,(14)0.00210.76910.47810.77350.59270.52030.37800.54010.53830.46820.30280.39700.45330.32510.63000.46590.66250.26570.41430.18030.34870.39900.50400.47480.51760.22770.45420.18740.38350.52030.25200.38580.06210.25930.54980.42010.41840.44030.37800.2967,(15)0.07430.70420.70410.34520.07050.06270.70240.07020.06980.53870.70380.65250.54500.22820.22840.49030.54550.50500.23120.54550.54550.39360.22880.21020.38810.38690.38690.44200.38710.5207.These weights of all attributes of respective consumables are evaluated using AHP method and the results are presented in Table 6.Table 6
Weights of the attributes from AHP method.
Attributes Filler alloy weights Electrode weights Shielding gas weights A 1 0.0326 0.0311 0.0428 A 2 0.0235 0.0447 0.1006 A 3 0.0476 0.1586 0.1595 A 4 0.1059 0.1036 0.0640 A 5 0.3313 0.2399 0.2504 A 6 0.1572 0.3542 0.3824 A 7 0.2306 0.0675 A 8 0.0709A weighted normalized decision matrix for filler alloy, electrode, and shielding gas is presented in matrices (16)(16)0.01740.01000.02410.06080.13230.07390.11120.04270.01030.01320.01990.03760.15680.08690.12830.03680.01920.01150.02410.05730.15190.08040.11970.03750.01480.00920.02410.04810.16860.05220.07700.03050.00810.00780.01130.02260.12740.05000.06410.0234,0.00010.03440.07550.07970.14170.18420.02550.04270.01670.02090.04780.04090.10830.11510.04250.03680.02060.01190.06550.01860.08330.14130.03400.03750.01610.01020.07180.01930.09170.18420.01700.03050.00190.01160.08690.04330.10000.15580.02550.0234,0.00320.07080.11230.02210.01770.02400.03010.00710.01110.03450.17620.24950.02330.02300.03640.03140.13660.19310.00990.05490.08700.02520.05730.08040.01660.03890.06170.02830.09690.1991.


## 3.2. Ranking Results

The relative closeness to the ideal solution hence can be found using (12). The ranks are assigned based on their “C” values and are given in Table 7. The larger the value of closeness the better the rank.Table 7
TOPSIS analysis result.
Filler alloy Electrode Shielding gas Alternates C i Rank Alternates C i Rank Alternates C i Rank ER5356 (C1) 0.8358 1 Pure tungsten (C1) 0.4084 4 Pure argon (C1) 0.7149 1 ER5556 (C2) 0.6184 3 2% thoriated (C2) 0.5789 2 Pure helium (C2) 0.2850 4 ER5183 (C3) 0.7205 2 2% ceriated (C3) 0.4745 3 25% argon + 75% helium (C3) 0.3280 3 ER5654 (C4) 0.3142 5 1.5% lanthanated (C4) 0.2835 5 75% argon + 25% helium (C4) 0.6719 2 ER5554 (C5) 0.3516 4 0.8% zirconiated (C5) 0.5869 1 50% argon + 50% helium (C5) 0.2363 5It can be concluded from Table7, filler alloy, ER5356 has the highest ranking followed by ER5183 while ER5654 is the least ranked material. In arc electrode selection problem the optimum arc electrode is 0.8% zirconiated electrode which is the best alternate as it has slightly higher “C” value than 2% thoriated electrode. Shielding gas analysis results indicate pure argon as the optimum consumable component closely followed by Ar-He gas blend as second best alternative. The block diagram for material selection application has been shown in Figure 2.Figure 2
Block diagram for material selection application.


## 3.3. Welding Experimentation

The butt welding of aluminum alloy of 5083-O and 6061-T651 using pulse TIG welding (Triton 220 AC/DC) is performed to establish the applicability and validity of the selection model.The chemical composition of filler alloys used has been depicted in Table8.Table 8
Chemical composition of filler alloys used.
Composition Si Mg Fe Cu Mn Cr Zn Ti Al ER5356 0.23 5.0 0.40 0.05 0.12 0.9 0.10 0.13 Balance ER5556 0.25 5.1 0.40 0.10 0.75 0.13 0.25 0.13 Balance ER5183 0.40 4.8 0.40 0.10 0.75 0.15 0.25 0.15 Balance ER5654 0.22 3.5 0.23 0.05 0.01 0.25 0.20 0.10 Balance ER5554 0.25 2.7 0.40 0.10 0.75 0.13 0.25 0.13 BalanceExperimental validation has been conducted using highest ranking materials, namely, ER5356 as filler alloy, 0.8% zirconiated electrode, and pure argon shielding gas as shown in Figure3.Figure 3
Flow diagram depicting applications of 5083-O and 6061-T651.


### 3.3.1. Radiography Examination

Welding was examined using radiography to check lack of penetration as shown in Figure4. No visual defects are observed in radiography film indicating proper fusion in weld joint leading to successful welding. 10 × 12 cm is the scale bar used.Figure 4
(a) Weld joint 5083-O + 6061 T-651. (b) Radiography.


### 3.3.2. Microstructure Characterizations

Microstructural characterization is important since various characteristics of phase particles especially mechanical properties, corrosion resistance, are dependent on form of Mg2Si in which it exists in a particular material.Microstructural characterization uses optical microscope and SEM (scanning electron microscope) images (3700N Hitachi) to check grain refining and formation of brittle phase shown in Figure5.Figure 5
Microstructure (200x) and SEM (5μm) images of base metal, heat affected zone, and fusion zone at both sides.Microstructure shows three different regions, that is, base metal, heat affected zone, and fusion zone on either side of weld. Figure6 shows fusion zone (FZ) region, in which fine equiaxed grains of aluminum solid solution containing soluble phase consisting of Mg2Si particles show proper grain refinement. Hence improved weld quality is accomplished.Figure 6
SEM image of Mg2Si particle.


## 3.3.1. Radiography Examination

Welding was examined using radiography to check lack of penetration as shown in Figure4. No visual defects are observed in radiography film indicating proper fusion in weld joint leading to successful welding. 10 × 12 cm is the scale bar used.Figure 4
(a) Weld joint 5083-O + 6061 T-651. (b) Radiography.


## 3.3.2. Microstructure Characterizations

Microstructural characterization is important since various characteristics of phase particles especially mechanical properties, corrosion resistance, are dependent on form of Mg2Si in which it exists in a particular material.Microstructural characterization uses optical microscope and SEM (scanning electron microscope) images (3700N Hitachi) to check grain refining and formation of brittle phase shown in Figure5.Figure 5
Microstructure (200x) and SEM (5μm) images of base metal, heat affected zone, and fusion zone at both sides.Microstructure shows three different regions, that is, base metal, heat affected zone, and fusion zone on either side of weld. Figure6 shows fusion zone (FZ) region, in which fine equiaxed grains of aluminum solid solution containing soluble phase consisting of Mg2Si particles show proper grain refinement. Hence improved weld quality is accomplished.Figure 6
SEM image of Mg2Si particle.


## 4. Conclusion

Selection of welding process consumables is important tasks of decision making in engineering design. There is a requirement to study the correlation between available material alternates and their attributes to produce a robust welding of aluminum alloys at the lowest overall cost. AHP-TOPSIS based MADM model makes it possible to provide both qualitative and quantitative study of intangible factors in welding process.The relevance of such decision support tool lies in enabling welding/design engineers to improvise the process management with minimum available data.In future research the approach can be used for selection of dissimilar metal alloys for common extrusion applications.



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