Mechanical Properties of Friction Stir Welded AA1050-H14 and AA5083-H111 Joint: Sampling Aspect

: Welding of dissimilar aluminium alloys has been a challenge for a long period until the discovery of the solid-state welding technique called friction stir welding (FSW). The discovery of this technique encouraged di ﬀ erent research interests revolving around the optimization of this technique. This involves the welding parameters optimization and this optimization is categorized into two classes, i.e., similar alloys and dissimilar alloys. This paper reports about the mechanical properties of the friction stir welded dissimilar AA1050-H14 and AA5083-H111 joint. The main focus is to compare the mechanical properties of specimens extracted from di ﬀ erent locations of the welds, i.e., the beginning, middle, and the end of the weld. The specimen extracted at the beginning of the weld showed low tensile properties compared to specimens extracted from di ﬀ erent locations of the weld. There was no certain trend noted through the bending results. All three specimens showed dimpled fracture, which is the characterization of the ductile fracture.


Introduction
Friction stir welding (FSW) is classified as one of the welding techniques that joins materials through heat generated during friction occurring between the tool shoulder and the workpieces [1]. The invention of this welding technique was based on the materials which were classified as un-weldable materials through conventional methods. Those classified materials included certain classes of aluminium alloys. Aluminium alloys are mostly used in many industries like aviation, shipbuilding, and automotive because of their light weight. The focus towards FSW has expanded such that it includes testing the capability of the technique in welding other materials that are outside the aluminium class. This includes the welding of copper and its alloys, titanium and magnesium and its alloys [2]. When the aluminium alloys are welded with the conventional technique, they are likely to have weld splitting on the joint line. The fusion welding of aluminium alloys is more difficult than the welding of steel due to their low melting point, softness, and so forth. The aluminium alloys sometimes bend and shrink when welded using conventional welding and those effects are caused by residual thermal stress [3].
In some materials, FSW possesses good metallurgical properties when compared to fusion welding, and this is caused by the microstructural modification that occurs during welding. Mishra and Ma [4] reported that to have a great weld and to avoid defects on the weld, it is important to take welding parameters, material flow, and heat generation into consideration during the welding process.
There are mainly four crucial steps that are involved during the performance of FSW, i.e., plunging, dwelling, welding, and pulling. The rotating tool is inserted into the butt joint slowly until the shoulder speeds. The microstructural analysis revealed that there was no rigorous mixing in the nugget region for both materials. The tensile properties of dissimilar materials (AA5052-AA6061) were much better compared to the properties of similar materials (AA6061-AA6061). Welding dissimilar aluminium alloys that are mechanically far apart has gained much attention and interest from researchers [19]. This includes the analysis of friction stir welding of dissimilar AA2017A-T451 and AA7075-T651 plates at a different tool rotation speed. The results revealed that the best tensile properties were achieved when AA2017A-T451 was on the retreating side. It was also established that the material that is located on the retreating side dominates the weld centre, and this is consistent with the results reported by other researchers [11,12,16]. Ranjith and Kumar [20] analysed the impact of joining two dissimilar aluminium alloys AA2014 T651 and AA6063 T651 by friction stir welding. They discovered that the tensile strength was better when the tool was offset towards AA2014 (advancing side). When it was offset towards AA6063 (retreating side), it resulted in insufficient heat generation on the advancing side, which then resulted in an incomplete fusion of AA2014. Sarsılmaz and Caydas [21] conducted a study on statistical analysis on mechanical properties of friction-stir-welded AA1050-H14/AA5083-H321 couples. The study investigated the effect of friction stir welding parameters focusing on rotational speed, traverse speed, and stirrer geometry. In their investigation, they discovered that traverse speed has a significant effect on UTS and nugget hardness. Their analysis also included the optimized welding parameters to be used in welding the said aluminium alloys.
The analysis of the effect of material positioning during FSW has gone outside the aluminium family. This includes the study which analyzed the effect of location variation in FSW of steel with different carbon content. It was discovered that the placement of the stronger material on the advancing side reduced the weld nugget size and increased the amount of martensite formation. The location of the strongest material on the advancing side led to higher temperature and stress due to the highest temperature on the advancing side [22]. It is evident from the literature that the FSW that involved materials that are mechanically apart involved mainly 2xxx as the weaker material. There are very few studies which utilized AA1xxx [21]. This paper reports on the mechanical properties of the weld produced by the friction stir welding technique using AA1050-H14 and AA5083-H111. The AA1050-H14 is mostly used in the chemical industry, automotive industry, reflectors, heat exchangers, and food industry [23]. The AA5083-H111 is widely used in the prevention of corrosion, hence used in shipbuilding. This alloy is also used in the automotive industry as well [24]. It was then crucial to analyze different aspects related to the joint formed from these two distinct materials. This was done so as to prepare the future application of these two materials in producing products and components. It then became crucial to analyze comparatively the mechanical behaviour of the joint in different locations. This type of analysis will give information regarding the best location for sampling the welds produced from the materials with unique properties and composition.

Experimental Procedure
The 6mm thick AA1050-H14 and AA5083-H111 plates were cut into 70 mm × 530 mm long strips using a guillotine cutting machine (see Figure 1). Kumbhar and Bhanumurthy [18] did a comparative study on friction stir welding of similar to dissimilar aluminium alloys, i.e., AA5052 to AA6061, and AA6061 to AA6061. The similar and dissimilar joints were produced at various combinations of tool rotation speeds and tool traverse speeds. The microstructural analysis revealed that there was no rigorous mixing in the nugget region for both materials. The tensile properties of dissimilar materials (AA5052-AA6061) were much better compared to the properties of similar materials (AA6061-AA6061). Welding dissimilar aluminium alloys that are mechanically far apart has gained much attention and interest from researchers [19]. This includes the analysis of friction stir welding of dissimilar AA2017A-T451 and AA7075-T651 plates at a different tool rotation speed. The results revealed that the best tensile properties were achieved when AA2017A-T451 was on the retreating side. It was also established that the material that is located on the retreating side dominates the weld centre, and this is consistent with the results reported by other researchers [11,12,16]. Ranjith and Kumar [20] analysed the impact of joining two dissimilar aluminium alloys AA2014 T651 and AA6063 T651 by friction stir welding. They discovered that the tensile strength was better when the tool was offset towards AA2014 (advancing side). When it was offset towards AA6063 (retreating side), it resulted in insufficient heat generation on the advancing side, which then resulted in an incomplete fusion of AA2014. Sarsılmaz and Caydas [21] conducted a study on statistical analysis on mechanical properties of friction-stir-welded AA1050-H14/AA5083-H321 couples. The study investigated the effect of friction stir welding parameters focusing on rotational speed, traverse speed, and stirrer geometry. In their investigation, they discovered that traverse speed has a significant effect on UTS and nugget hardness. Their analysis also included the optimized welding parameters to be used in welding the said aluminium alloys.
The analysis of the effect of material positioning during FSW has gone outside the aluminium family. This includes the study which analyzed the effect of location variation in FSW of steel with different carbon content. It was discovered that the placement of the stronger material on the advancing side reduced the weld nugget size and increased the amount of martensite formation. The location of the strongest material on the advancing side led to higher temperature and stress due to the highest temperature on the advancing side [22]. It is evident from the literature that the FSW that involved materials that are mechanically apart involved mainly 2xxx as the weaker material. There are very few studies which utilized AA1xxx [21]. This paper reports on the mechanical properties of the weld produced by the friction stir welding technique using AA1050-H14 and AA5083-H111. The AA1050-H14 is mostly used in the chemical industry, automotive industry, reflectors, heat exchangers, and food industry [23]. The AA5083-H111 is widely used in the prevention of corrosion, hence used in shipbuilding. This alloy is also used in the automotive industry as well [24]. It was then crucial to analyze different aspects related to the joint formed from these two distinct materials. This was done so as to prepare the future application of these two materials in producing products and components. It then became crucial to analyze comparatively the mechanical behaviour of the joint in different locations. This type of analysis will give information regarding the best location for sampling the welds produced from the materials with unique properties and composition.

Experimental Procedure
The 6mm thick AA1050-H14 and AA5083-H111 plates were cut into 70 mm × 530 mm long strips using a guillotine cutting machine (see Figure 1).  The two dissimilar plates were fixed on the backplate of the semi-automated milling machine (FSW machine), as shown in Figure 2. The AA5083-H111 was kept on the retreating side throughout the experiments, while AA1050-H14 was on the advancing side. This kind of material location was followed based on the recommendation from the literature [11,12,16,19,25,26]. The plates were fixed on the machine's backplate by eight clamps. The function of clamps was to make sure the plates did not move apart when the rotating pin was in motion. The two dissimilar plates were fixed on the backplate of the semi-automated milling machine (FSW machine), as shown in Figure 2. The AA5083-H111 was kept on the retreating side throughout the experiments, while AA1050-H14 was on the advancing side. This kind of material location was followed based on the recommendation from the literature [11,12,16,19,25,26]. The plates were fixed on the machine's backplate by eight clamps. The function of clamps was to make sure the plates did not move apart when the rotating pin was in motion. The plates were then friction stir welded using a high carbon steel (H13) tool shown in Figure 3. The tool was machined using a lathe machine and was heat-treated to about 50HRC. The profile of the pin was triangularly threaded with a 20 mm shoulder diameter and 6 mm pin diameter. The triangular threaded pin had a 1mm pitch and the height of 5.8 mm. The FSW parameters used in this study are presented in Table 1, and these parameters were chosen based on various speed test combinations performed prior to the main welding. However, those trial results are not included in this work since they are not part of the paper's focus.

Rotational Speed (rpm) Traverse Speed (mm/min) Tilt Angle (°)
1000 30 2 The plates were then friction stir welded using a high carbon steel (H13) tool shown in Figure 3. The tool was machined using a lathe machine and was heat-treated to about 50HRC. The profile of the pin was triangularly threaded with a 20 mm shoulder diameter and 6 mm pin diameter. The triangular threaded pin had a 1mm pitch and the height of 5.8 mm. The FSW parameters used in this study are presented in Table 1, and these parameters were chosen based on various speed test combinations performed prior to the main welding. However, those trial results are not included in this work since they are not part of the paper's focus.   Figure 4 shows the friction stir welding of 6 mm thick AA1050 and AA5083 plates. Stage 1 shows two plates ready for welding. Stage 2 shows the rotating tool plunged into the two pieces being welded, i.e., AA1050-H14 and AA5083-H111. Stage 3 shows the welded part of the plates. Stage 4 shows the end of FSW and the unplunging of the tool. The finished product is clearly shown in Figure  5. The nominal chemical composition for materials used in this study is presented in Table 2. The chemical composition was measured using the BELEC COMPACT PORT HLC spectrometer (Belec Spektrometrie Opto-Elektronik GmbH, Georgsmarrienhutte, Germany) according to ASTM E716-16 standard. These chemical compositions were in the range of those reported in the literature [16,21,27].  Figure 4 shows the friction stir welding of 6 mm thick AA1050 and AA5083 plates. Stage 1 shows two plates ready for welding. Stage 2 shows the rotating tool plunged into the two pieces being welded, i.e., AA1050-H14 and AA5083-H111. Stage 3 shows the welded part of the plates. Stage 4 shows the end of FSW and the unplunging of the tool. The finished product is clearly shown in Figure 5. The nominal chemical composition for materials used in this study is presented in Table 2. The chemical composition was measured using the BELEC COMPACT PORT HLC spectrometer (Belec Spektrometrie Opto-Elektronik GmbH, Georgsmarrienhutte, Germany) according to ASTM E716-16 standard. These chemical compositions were in the range of those reported in the literature [16,21,27].

Welded Joint Analysis
This section describes the mechanical and microstructural analysis of the welded joint. This includes the use of the tensile test machine, microstructure analysis, bending test, and scanning electron microscope (SEM). It should be noted that the friction stir welded joint had start, middle, and end points. The specimens were all labeled A, B, and C. Label A indicated the specimens cut at the beginning of the joint, specimens cut in the middle were labeled B, while C symbolized the specimens cut at the end of the joint. This format was followed throughout the performance of the tests.

Tensile Test
The machine that was used for the tensile test was the Hounsfield tensometer (universal testing machine). The tensile test was performed using the ASTM E8 standard. The tensile test specimens were cut perpendicular to the welding direction (see Figure 6). The tensile test specimens were designed according to the ASTM E8M-04 standard [28] for accurate dimensions. The specimens were cut using CNC wire cutters and the coordinates for cutting specimens were manually generated using 2-D drawings in Solidworks, shown in Figure 7. This method of cutting was selected because it does not induce heat during cutting. There were three tensile specimens extracted from different locations of the plate (see Figure 6). The extensometer was used to capture the data relevant to the joint.

Welded Joint Analysis
This section describes the mechanical and microstructural analysis of the welded joint. This includes the use of the tensile test machine, microstructure analysis, bending test, and scanning electron microscope (SEM). It should be noted that the friction stir welded joint had start, middle, and end points. The specimens were all labeled A, B, and C. Label A indicated the specimens cut at the beginning of the joint, specimens cut in the middle were labeled B, while C symbolized the specimens cut at the end of the joint. This format was followed throughout the performance of the tests.

Tensile Test
The machine that was used for the tensile test was the Hounsfield tensometer (universal testing machine). The tensile test was performed using the ASTM E8 standard. The tensile test specimens were cut perpendicular to the welding direction (see Figure 6). The tensile test specimens were designed according to the ASTM E8M-04 standard [28] for accurate dimensions. The specimens were cut using CNC wire cutters and the coordinates for cutting specimens were manually generated using 2-D drawings in Solidworks, shown in Figure 7. This method of cutting was selected because it does not induce heat during cutting. There were three tensile specimens extracted from different locations of the plate (see Figure 6). The extensometer was used to capture the data relevant to the joint.  Table 2. Chemical composition of AA1050-H14 and AA5083-H111 (wt.%) [16,21,30].

Material
Si

Welded Joint Analysis
This section describes the mechanical and microstructural analysis of the welded joint. This includes the use of the tensile test machine, microstructure analysis, bending test, and scanning electron microscope (SEM). It should be noted that the friction stir welded joint had start, middle, and end points. The specimens were all labeled A, B, and C. Label A indicated the specimens cut at the beginning of the joint, specimens cut in the middle were labeled B, while C symbolized the specimens cut at the end of the joint. This format was followed throughout the performance of the tests.

Tensile Test
The machine that was used for the tensile test was the Hounsfield tensometer (universal testing machine). The tensile test was performed using the ASTM E8 standard. The tensile test specimens were cut perpendicular to the welding direction (see Figure 6). The tensile test specimens were designed according to the ASTM E8M-04 standard [28] for accurate dimensions. The specimens were cut using CNC wire cutters and the coordinates for cutting specimens were manually generated using 2-D drawings in Solidworks, shown in Figure 7. This method of cutting was selected because it does not induce heat during cutting. There were three tensile specimens extracted from different locations of the plate (see Figure 6). The extensometer was used to capture the data relevant to the joint.  The specimens were tensile tested until they fractured.

Microstructure Analysis
The microstructure analysis was performed using the Nikon Eclipse L150 microscope (Nikon, Tokyo, Japan). The microstructure was observed under a polarized slider with an Axiocam 105 colour camera for acquiring the pictures. The specimens were cut into 26 × 8 × 6 mm using the CNC wire cutter and prepared for analysis using Keller's reagent etchant.

Bending Test
Three-point bending tests were conducted using the same Hounsfield tensometer previously used for the tensile tests. The performance of the bending test was based on the ASTM E290-97a standard. There were six rectangular-shaped specimens prepared for bending tests. The bending tests were performed on the face and the root of the joint. The three specimens presented in Figure 8 show the face of the joint (the surface that was in contact with the tool shoulder) and another three presented in Figure 9 show the root of the joint (the surface that was in contact with the backplate). For comparative purposes, the bending test was also performed on parent materials. The specimens were tensile tested until they fractured.

Microstructure Analysis
The microstructure analysis was performed using the Nikon Eclipse L150 microscope (Nikon, Tokyo, Japan). The microstructure was observed under a polarized slider with an Axiocam 105 colour camera for acquiring the pictures. The specimens were cut into 26 × 8 × 6 mm using the CNC wire cutter and prepared for analysis using Keller's reagent etchant.

Bending Test
Three-point bending tests were conducted using the same Hounsfield tensometer previously used for the tensile tests. The performance of the bending test was based on the ASTM E290-97a standard. There were six rectangular-shaped specimens prepared for bending tests. The bending tests were performed on the face and the root of the joint. The three specimens presented in Figure 8 show the face of the joint (the surface that was in contact with the tool shoulder) and another three presented in Figure 9 show the root of the joint (the surface that was in contact with the backplate). For comparative purposes, the bending test was also performed on parent materials.

Scanning Electron Microscope (SEM)
The SEM used was the Zeiss Auriga (Carl Zeiss Microscopy GmbH Co., Germany). Prior to the analysis, the samples were coated with a layer of carbon to ensure sufficient conductivity during analysis. The results obtained are presented and explained in the next section.

Results and Discussion
The detailed discussions of the results obtained from the various tests performed are presented in this section. The results obtained include the tensile test, bending test, microstructure and SEM analysis.

Microstructure
The FSW joint was characterized by general unique zones as shown in Figure 9. Those zones included the stir zone (SZ) around the weld centre line, the thermo-mechanically affected zone (TMAZ) on both sides of the weld nugget/stir zone, the heat-affected zone (HAZ), which surrounded the TMAZ, and the non-affected base metal (BM) [12][13][14][15][16][17][18]. The regions originated from the material flow behaviour caused by the tool rotation. The macroscopic and microscopic patterns of the three specimens were similar, hence one pattern is presented to avoid duplication. Figure 9a shows the macroscopic view of the joint with its thermal zones. There are no defects visible on the joint. This suggests that the welding was performed successfully [21,29]. Figure 9b,c shows the micrographs of base metals AA1050-H14 and AA5083-H111, respectively. Figure 9d shows the microscopic view of the AA1050-H14 pulled towards the stir zone, and this morphology is called hook defect [30]. Figure  9e shows rotational traces of the materials at the stir zone. Figure 9f shows the magnified morphology of the stir zone. The magnified view shows the refined grain structures at the stir zone. The average grain size for the base metal AA1050-H14 was about 29 µm while the average grain size of AA5083-

Scanning Electron Microscope (SEM)
The SEM used was the Zeiss Auriga (Carl Zeiss Microscopy GmbH Co., Germany). Prior to the analysis, the samples were coated with a layer of carbon to ensure sufficient conductivity during analysis. The results obtained are presented and explained in the next section.

Results and Discussion
The detailed discussions of the results obtained from the various tests performed are presented in this section. The results obtained include the tensile test, bending test, microstructure and SEM analysis.

Microstructure
The FSW joint was characterized by general unique zones as shown in Figure 9. Those zones included the stir zone (SZ) around the weld centre line, the thermo-mechanically affected zone (TMAZ) on both sides of the weld nugget/stir zone, the heat-affected zone (HAZ), which surrounded the TMAZ, and the non-affected base metal (BM) [12][13][14][15][16][17][18]. The regions originated from the material flow behaviour caused by the tool rotation. The macroscopic and microscopic patterns of the three specimens were similar, hence one pattern is presented to avoid duplication. Figure 9a shows the macroscopic view of the joint with its thermal zones. There are no defects visible on the joint. This suggests that the welding was performed successfully [21,29]. Figure 9b,c shows the micrographs of base metals AA1050-H14 and AA5083-H111, respectively. Figure 9d shows the microscopic view of the AA1050-H14 pulled towards the stir zone, and this morphology is called hook defect [30]. Figure 9e shows rotational traces of the materials at the stir zone. Figure 9f shows the magnified morphology of the stir zone. The magnified view shows the refined grain structures at the stir zone. The average grain size for the base metal AA1050-H14 was about 29 µm while the average grain size of AA5083-H111 base metal was about 7.3 µm. The average grain size for the stir zone was about 9.35 µm. The average grain size for the stir zone is close to the average grain size for AA5083-H111 base metal.
Metals 2020, 10, x FOR PEER REVIEW 10 of 16 H111 base metal was about 7.3 µm. The average grain size for the stir zone was about 9.35 µm. The average grain size for the stir zone is close to the average grain size for AA5083-H111 base metal.  Figure 10 shows the fractured specimens post tensile tests. It was observed that the fracture occurred on the advancing side (AA1050) of the specimen. This behaviour suggests that the weld joint was mechanically stronger than the AA1050 alloy [11,12,28]. This also suggests that the welded joint was dominated by AA5083-H111, hence it was stronger [16,[29][30][31].  Figure 10 shows the fractured specimens post tensile tests. It was observed that the fracture occurred on the advancing side (AA1050) of the specimen. This behaviour suggests that the weld joint was mechanically stronger than the AA1050 alloy [11,12,28]. This also suggests that the welded joint was dominated by AA5083-H111, hence it was stronger [16,[29][30][31]. Figure 10 shows the fractured specimens post tensile tests. It was observed that the fracture occurred on the advancing side (AA1050) of the specimen. This behaviour suggests that the weld joint was mechanically stronger than the AA1050 alloy [11,12,28]. This also suggests that the welded joint was dominated by AA5083-H111, hence it was stronger [16,[29][30][31].   19 MPa, respectively. It should be noted that all the specimens were fractured by the HAZ region of the AA1050-H14 side. The HAZ region is known to have a negative impact towards the UTS of a material due to the coarsened grains that are normally associated with this region [19,20,[30][31][32][33]. This is suggested to be the cause of the lower UTS for the three specimens compared to the parent materials. This assumption is in line with the grain variations observed during microstructural analysis. The percentage elongation was found to be 19%, 25%, and 26% for specimen A, B, and C, respectively. These indicate that the FSW specimens B and C were more ductile compared to the specimen A and AA1050-H14 parent material, but less ductile compared to parent material AA5083.  Figure 11 shows the tensile test-strain curve of AA1050-H14, AA5083, and FSW specimens A, B, and C. The UTS of the parent material AA5083 was larger than that of the parent material AA1050-H14 and of the FSW specimens. Specimen A, which was the first specimen from the welded plate, was the weakest while specimens B and C were close to each other. This behaviour was assumed to be caused by insufficient heat input at the beginning of the weld. The temperature stabilized from the middle to the end of the plate, hence improved UTS. Figure 11 shows the tensile test-strain curve of AA1050-H14, AA5083, and FSW specimens A, B, and C. The UTS of the parent material AA5083 was larger than that of the parent material AA1050-H14 and of the FSW specimens. Specimen A, which was the first specimen from the welded plate, was the weakest while specimens B and C were close to each other. This behaviour was assumed to be caused by insufficient heat input at the beginning of the weld. The temperature stabilized from the middle to the end of the plate, hence improved UTS.  Figures 12 and 13 are the post-bending test specimens for FSW and parent materials. The reddish-brown line appearing on specimens in Figure 12a,b indicates the center of the joint. The face and the root bending occurred towards the advancing side of the joint. This behaviour suggests that the joint was mechanically stronger compared to AA1050-H14, hence bending occurred on the advancing side. This behaviour is in agreement with the behaviour observed in the tensile analysis.

Bending Test
Figures 12 and 13 are the post-bending test specimens for FSW and parent materials. The reddish-brown line appearing on specimens in Figure 12a,b indicates the center of the joint. The face and the root bending occurred towards the advancing side of the joint. This behaviour suggests that the joint was mechanically stronger compared to AA1050-H14, hence bending occurred on the advancing side. This behaviour is in agreement with the behaviour observed in the tensile analysis. The post-bending results showed the tested specimens without failure. This means that the welded materials bonded well during welding. The post-bending results showed the tested specimens without failure. This means that the welded materials bonded well during welding.      Figures 14 and 15 show bending stress and strain curves of the joint, together with parent materials. As it has been mentioned before that all the welded specimens bent on AA1050-H14, the flexural stresses for both face and root were within the range of that of AA1050-H14 (see Table 4). The average stress for face and root was 218.94 MPa and 259 MPa, respectively. These values suggest that the root side of the weld was stronger than that of the face. This could be caused by the fact that the lower side of the weld was exposed to the restricted downward movement due to bed backing plate. The flexural stress values were comparatively higher than the tensile values and this was due to higher temperatures involved during FSW.  Figures 14 and 15 show bending stress and strain curves of the joint, together with parent materials. As it has been mentioned before that all the welded specimens bent on AA1050-H14, the flexural stresses for both face and root were within the range of that of AA1050-H14 (see Table 4). The average stress for face and root was 218.94 MPa and 259 MPa, respectively. These values suggest that the root side of the weld was stronger than that of the face. This could be caused by the fact that the lower side of the weld was exposed to the restricted downward movement due to bed backing plate. The flexural stress values were comparatively higher than the tensile values and this was due to higher temperatures involved during FSW.   Figures 14 and 15 show bending stress and strain curves of the joint, together with parent materials. As it has been mentioned before that all the welded specimens bent on AA1050-H14, the flexural stresses for both face and root were within the range of that of AA1050-H14 (see Table 4). The average stress for face and root was 218.94 MPa and 259 MPa, respectively. These values suggest that the root side of the weld was stronger than that of the face. This could be caused by the fact that the lower side of the weld was exposed to the restricted downward movement due to bed backing plate. The flexural stress values were comparatively higher than the tensile values and this was due to higher temperatures involved during FSW.

Scanning Electron Microscopy (SEM)
It should be noted that the fractured surface for base metals was studied comparatively with specimen C. The elimination of other specimens was due to the fact that there was no distinction on the surface morphology for the other specimens. Figures 16 and 17 show the surface morphologies of the base metals and weldment (joint). All the specimens showed a cup-like dimpled fracture, which is a characterization of ductile failure mode [30,32,33]. The similarity in surface fracture suggests that the ductility of the materials involved in the joint formation was preserved post welding even though there was some percentage of elongation variation.

Scanning Electron Microscopy (SEM)
It should be noted that the fractured surface for base metals was studied comparatively with specimen C. The elimination of other specimens was due to the fact that there was no distinction on the surface morphology for the other specimens. Figures 16 and 17 show the surface morphologies of the base metals and weldment (joint). All the specimens showed a cup-like dimpled fracture, which is a characterization of ductile failure mode [30,32,33]. The similarity in surface fracture suggests that the ductility of the materials involved in the joint formation was preserved post welding even though there was some percentage of elongation variation.

Conclusions
The absence of voids or defects on the macrostructure of the joint suggests the success of welding the two dissimilar aluminium alloys (AA1050-H14 and AA5083-H111). The UTS of the base metals was found to be higher than the UTS of the tested specimens. In addition to this, the specimen extracted at the beginning of the weld exhibited the lowest UTS compared to the specimens extracted from other locations of the weld. The ductility of the specimens fluctuated between that of the parent materials. The fracture location was found to be consistent with the one reported in the literature [11,12,16]. This kind of failure is due to the coarsened grain found in the location of failure (AA1050-

Conclusions
The absence of voids or defects on the macrostructure of the joint suggests the success of welding the two dissimilar aluminium alloys (AA1050-H14 and AA5083-H111). The UTS of the base metals was found to be higher than the UTS of the tested specimens. In addition to this, the specimen extracted at the beginning of the weld exhibited the lowest UTS compared to the specimens extracted from other locations of the weld. The ductility of the specimens fluctuated between that of the parent materials. The fracture location was found to be consistent with the one reported in the literature [11,12,16]. This kind of failure is due to the coarsened grain found in the location of failure (AA1050-

Conclusions
The absence of voids or defects on the macrostructure of the joint suggests the success of welding the two dissimilar aluminium alloys (AA1050-H14 and AA5083-H111). The UTS of the base metals was found to be higher than the UTS of the tested specimens. In addition to this, the specimen extracted at the beginning of the weld exhibited the lowest UTS compared to the specimens extracted from other locations of the weld. The ductility of the specimens fluctuated between that of the parent materials. The fracture location was found to be consistent with the one reported in the literature [11,12,16]. This kind of failure is due to the coarsened grain found in the location of failure (AA1050-H14 HAZ region). The characteristic hook defect on the side of the weaker material was also observed during the microstructural analysis [29][30][31]33]. The morphology of the fracture surface indicated ductile failure mode, which was characterized by cup-like dimples for all the specimens.
Author Contributions: Authors have contributed equally to this work. All authors have read and agreed to the published version of the manuscript.
Funding: This research received no external funding.