An Investigation To Achieve a Good Surface Integrity in WEDM of Ti-6242 Super Alloy

Ti-6242 is a super alloy which exhibits the best creep resistance among available titanium alloys and is widely used in the manufacture by WEDM of aircraft engine turbomachinery components. However, the nal quality of wire EDMed surface is a great challenge as it is affected by various factors that need optimization for surface integrity and machine eciency improvement. The aim of this study is to investigate the effect of a set of cutting process parameters such as pulse on time (T on ), servo voltage (U), feed rate (S) and ushing pressure (p) on surface roughness (SR) when machining Ti-6242 super alloy by WEDM process using a brass tool electrode and deionized water as a dielectric uid. WEDM experiments were conducted, and SR (Ra) measurement was carried out using a 3D optical surface roughness-meter (3D–SurfaScan). As a tool to optimize cutting parameters for SR improvement, Taguchi's signal ‐ to ‐ noise ratio (S/N) approach was applied using L 9 (3^4) orthogonal array and Lower-The-Better (LTB) criteria. Substantially, the ndings from current investigation suggest the application of the values 0.9 µs, 100V, 29 mm/min, and 60 bar for T on , U, S and p cutting parameters, respectively, for producing a good surface nish quality. Percent contributions of the machining parameters on SR (Ra) assessed based on ANOVA analysis are 62.94%, 20.84%, 11.46% and 4.74% for U, S, T on and p, respectively. Subsequently, accurate predictive model for SR (Ra) is established based on response surface analysis (RSA). The contour plots for SR (Ra) indicate that when ushing pressure p converges to a critical value (80 bar), a poor-quality surface nish is highly expected with the excessive increase in U and S. Electron microscope scanning (SEM) observations have been performed on machined surface for a wide range of cutting parameters to characterize wire EDMed surface of Ti-6242. SEM micrographs indicate that the machined surface acquires a foamy structure and shows white layer and machining-induced damage that the characteristics are highly dependent on cutting parameters. At high servo-voltage, the decrease in pulse on time T on and feed rate S results in a large decrease in overall machining-induced surface damage. Moreover, for high servo-voltage and feed rate levels, it has been observed that pulse on time could play a role of controlling the surface microcracks density. In fact, the use of a low pulse duration of cut combined with high servo-voltage and feed rate has been shown to inhibit surface microcracks formation giving the material surface a better resistance to cracking than at high pulse duration. (S/N) approach. Accordingly, L9 (3^4) orthogonal array ‐ based experimentation was designed, and Lower-The-Better (LTB) criteria was applied. Percent contributions of each machining parameter on SR (Ra) has been determined using ANOVA analysis, and a quadratic model expressed with U, T on , S and P to predict SR (Ra) has been established using response surface analysis (RSA). SEM observations were performed to examine microstructural alterations and machining-induced surface-breaking cracks in wire EDMed surface of Ti-6242 super alloy. The effect of the involved machining parameters on white layer thickness and surface microcracks density has been discussed deeply. During this investigation it was established that:


Introduction
One of the very plentiful metallic material on World, titanium is just lately employed in manufacturing, since an effective industrialization way was established just in the mid-twentieth century. Nowadays, titanium is extensively exploited in aerospace industry owing to its good mechanical and chemical properties mainly its high strength and good corrosion resistance, along with lightness (density of about 50 % less than steel). The airplane engines aeronautic components made of titanium alloy may operate at low to rationally elevated temperatures [1]. The greatest advantage compared to aluminum alloys that are also characterized by their low density, lies in operating temperature of the titanium alloys components which may reach very high levels, close to 600 °C, depending on the alloying elements [2].
Despite the relevant mechanical and chemical properties of titanium alloys, the machinability constitutes a great disadvantage and categorized as being poor. Therefrom, the complexity of conventional machining of titanium alloy parts which requires an extensive process time along with present high tool cost [3].
In the aerospace industry, some di culties are encountered in manufacturing of the monolithic parts. Indeed, most commonly used materials are heat-resistant materials such as Ti-based alloy (6242) and nickel or cobalt based super alloys [4].
However, during the last 10 years, research and development R&D on other machining technologies of titanium alloys has included both conventional and non-conventional methods of material processing involving abrasive water jet cutting, electrochemical/electrolytic point grinding (ECPG), abrasive methods such as cup grinding, new con gurations of form milling including both indexable solid and tooling, laser cutting, and remarkably electrical discharge machining (EDM) [5][6][7][8][9][10][11].
The EDM process is a non-contact manufacturing process which occurs between workpiece and electrode tool separated by a stream of insulating dielectric uid, which can generate material removal mainly by erosion phenomena regardless of the thermo-mechanical properties of the workpiece material. The eroded material portion which is not really removed and resolidi ed on the machined surface forms a super cial layer, so-called white layer, displaying distinct mechanical properties than original base material [12]. However, phenomenon involved in EDM process and achieved surface integrity have been traditionally challenged and researchers still debate on some aspects [13]. The surface alterations generated by EDM process have an important in uence on surface integrity as stated in several studies [12][13][14][15]. Hence the importance of optimizing the whole of the factors involved in EDM process namely, the type of EDM process (WEDM or SEDM), the job and electrode tool materials, the machinery parameters, the characteristics of the employed dielectric liquid along with material removal rate MRR, kerf size, wire failure and wire wear rate frequency, cutting rate etc. to limit the time of machining and cost, and increasing productivity while guaranteeing good nish quality of the products machined surface [16][17][18][19][20][21].Among the titanium alloys used in manufacturing industries, we nd the heat resistant Ti-6442 super alloy. The applications include aeronautical industries in particular turbines blades, parts of precision racing engine, the discs of hot section gas turbine parts, impellers, engine valves.
As being a super alloy, the machining of Ti-6442 by conventional processing techniques is di cult, hence the need for un-conventional process such as the EDM. Despite the implication of Ti-6242 super alloy in large industrial applications such as mentioned above and despite the signi cative in uence of surface quality or roughness of EDMed components on e ciency of the machines [22], the study of the effect of process parameters in EDM process of this titanium alloy for the purpose of process optimization and surface quality improvement has been established by few studies. It has been observed from the exhaustive literature review that most of the investigations in EDM process of Ti-6242 super alloy has focused on the optimization of quality characteristics such as material removal rate MRR, over cut, tool wear rate and surface roughness as representing important indicators for machined surface quality and to assess the effectiveness of the process. Perumal et al. (2020) [23] studied the effect of discharge current, spark on time and tool diameter on MRR, over cut and tool wear rate in EDM of Ti-6242. In an earlier study, Perumal et al. (2019) [18] have analyzed statistically, for the same grade of titanium, the surface roughness and used SEM analysis to characterize surface integrity in terms of microstructure and surface cracks.
On the other hand, some works have investigated the WEDM of Ti-6242. Recently, Shather et al. (2021) [24] have investigated the nano dielectric effect in WEDM of Ti-6242 to improve process e ciency in particular increasing the MRR. Prasanna et al (2021) [25] have studied the effect of some WEDM process inputs mainly pulse on time, voltage, and wire feed rate on MRR and surface integrity of Ti-6242. The obtained results show that surface roughness is highly affected by wire feed rate and voltage, and the MRR in WEDM of Ti-6242 is improved when the pulse on time is increased. In a recent work, Perumal et al. [26] have machined the Ti-6242 by WEDM process to study the effect of pulse on-time, pulse off time, wire feed and wire tension on MRR and surface roughness. Accordingly, various approaches have been employed for predicting and optimizing process parameters in EDM and WEDM of Ti-6242. These approaches are based on the notion of metal machining, design of experiment (DOE) method, Taguchi method and the response surface methodology approach (RSA) [19,23,[25][26][27][28][29]. For instance, to improve the MRR and reduce the over cut and tool wear rate in EDM of Ti-6242, Taguchi based grey relational analysis method using L27 orthogonal array with multi response optimization has been used by Perumal et al.
(2020) [23]. Taguchi method was employed by Prasanna et al (2021) [25] to identify optimal parameter combination for attaining minimal surface roughness in WEDM of Ti-6242. Even though being a material with very strong implication in industrial applications, the investigation of the surface roughness and the in uencing setting parameters in WEDM of Ti-6242 super alloy has been presented by few studies and resultantly captured little interest. Apart from a few studies dealing with surface integrity optimization in WEDM of Ti-6242 such those indicated above, most of the researchers investigated only micro-structure and mechanical properties.
In this study, an attempt was made to manufacture the Ti-6242 titanium super alloy by WEDM using a brass tool electrode and deionized water as dielectric uid to study the in uence of setting parameters of primary noteworthiness such as pulse on time (T on ), servo voltage (U), feed rate (S) and ushing pressure (p) on machined surface quality. Accordingly, Taguchi's signal-to-noise ratio approach is employed to create plan for assessment of surface roughness considering the involved cutting settings input. Subsequently, SEM micrographs of machined surface obtained for various cutting settings are taken to examine microstructural alterations and surface damage characteristics in WEDM processing of the Ti-6242 super alloy. Thus, effect of cutting parameters on surface integrity has been deeply discussed.

1. Workpiece material and machining
The material investigated in present work is the Ti-6242 titanium alloy. This material is an alpha-beta titanium alloy; it exhibits good mechanical strength and offers a su ciently high creep resistance to temperatures as high as 550°C. Ti-6242 titanium alloy also offers fair weldability and good corrosion resistance. The chemical compositions, thermo-mechanical proprieties and microstructure (asreceived) of the Ti-6242 super alloy are given in Table 1  The machining of Ti-6242 super alloy is conducted on a (Robo l 190) CNC wire EDM machine (Figure 1 (b)). A 0.25mm brass wire-rod (see Table 2 for material properties) and deionized water are used as tool electrode and dielectric medium, respectively, in cutting by wire EDM of a Ti-6242 rectangular workpiece to several samples (12*8*3mm 3 ) according to experimental con guration illustrated in Figure 1 (c).
Surface integrity in WEDM of Ti-6242 super alloy is studied through the examination of surface roughness along with machining-induced damage for Ti-6242 manufactured samples according to the strategy described below.

Strategy
For improving the quality characteristics and surface integrity in WEDM of Ti-6242 super alloy, we propose in present study following the various steps of diagram of Figure 2 where Taguchi method is employed including all of Signal-to-Noise ratio (S/N) approach, analysis of variance (ANOVA) and response surface analysis (RSA). In this work, 3 sets of 4 cutting parameters that are servo voltage or tension (U: the minimum input voltage value), pulse on time (T on ), feed rate or advance speed (S), and injection pressure or ushing pressure (p) are considered. Flushing (injection) pressure usually allows avoiding any undesirable effect from contact between the cut surface and debris, resulting in a good surface nish quality. WEDM experiments that the setup is illustrated in schematic diagram of Figure 1-a are conducted to investigate the effect of the process variables involved on surface roughness (Ra) during WEDM of Ti-6242 titanium alloy ( Figure 3). In fact, arithmetic surface roughness (Ra) as being the most signi cant constituent of the surface integrity is in uenced by several machining factors and plays a crucial role on the e ciency of aerospace components such as for instance turbomachinery blades as reported by [22] [32]. Hence, the need of surface roughness (Ra) improvement based on optimization of the process input factors. The cutting parameters ranges level along with the initial values for the machining settings have been chosen in the manufacturer's manual suggested for the investigated grade of titanium alloy. In Table 3 are reported the control factors, their symbols and their designated ranges employed in present work. of experiments, OA is applied in the Taguchi method. However, the S/N ratio is employed to assess the quality characteristics deviation from the desired values, including the Higher-The-Better (HTB), Nominal-The-Better (NTB) and Smaller-The-Better (STB) criteria. In this study we aim to optimize the surface roughness (Ra) so that the most objective type of objective function: Smaller-The-Better (STB), is considered herein. The exact relationship between the S / N ratio and the signal according to STB objective function is given by: where n is the number of experiments, and Y i is the value of the Ra.
In this study the standard experimental model is based on Taguchi Method. Thereby, an orthogonal matrix L9 (3^4) (see Table 4) described in GS peace [33], including a basic design involving four control factors namely startup voltage (U), pulse on time (T on ), feed rate (S) and ushing pressure (p) with three levels each, is used. Using the levels combination for each control factor shown in Table 3, a total of nine experimental runs should be conducted (Table 4). In this work, the roughness (Ra) represents the only machining characteristic to be investigated based on Taguchi method. WEDM experiments on Ti-6242 were performed to examine the signi cance of the input factors U, T on , S and P on surface roughness (Ra). The latter was assessed using a 3D optical surface roughness-meter (3D-SurfaScan), and the examined area was 2 * 1 mm 2 . The nal experimental results are stated in Table 4.

Results And Discussion
Since it is always advantageous to minimize the surface roughness, the S/N ratio was applied to determine the optimum cutting parameters for a good surface nish quality in WEDM of Ti-6242 titanium alloy. Accordingly, Minitab statistical software is employed in all the analysis plots and designs. The response tables for S/N ratio and means on surface roughness of Ti-6242 titanium alloy are given in Tables 5 and 6, respectively. In Figure 4 and 5 are plotted the main effects for S/N ratio and means on surface roughness (Ra) versus all the input factors, respectively.
The Figures 4-a, b, c, and d demonstrate the in uence of the four input factors (U, T on , S and P) on the mean S/N ratios, respectively. It can be observed that the lines joining data points of different levels have different slopes for servo voltage (U), pulse on time (T on ), feed rate (S) and ushing pressure (p) input factors. Hence, the levels in uence differently the surface roughness. Table 5 and gure 4 are obtained according to STB criterion. The level with the greatest S/N ratio is considered the optimal level of the machining parameters. The better combination of input factors can be now selected from graph of Figure 4 (see also Table 5 (smaller is best)). It can be observed that the best combination is formed by the levels (L2, L2, L1, L1) for input factors (U, T on , S and P), respectively. Therefore, the lowest surface roughness (Ra) is achieved at the values 100V, 0.9 µs, 29mm/min and 60 bar for U, T on , S and p, respectively in WEDM of Ti-6242 titanium alloy by brass wire and deionized water. Response Table for Signal-to-noise Figure 5-a shows that when the voltage U increases from 80 to 100V, the mean of surface roughness (Ra) decreases slightly, however, the increase in servo voltage from 100 to 120V results in signi cant rise in the mean of surface roughness. It can be seen also from the graph of Figure 5-c that mean of surface roughness increases at rst with the increase in advanced speed S from 29 to 36, thereafter it leaps as S rises from 36 to 43mm/min.
On the other hand, it can be observed from Table 6 that the effect of machining parameters U and S on mean of surface roughness (Ra) in WEDM of Ti-6242 alloy using brass wire and deionized water dominates the effect of T on and P. Indeed, the higher the slope values in the main effects plot, the higher the values of delta in the response table for means. The rank directly represents the level of input factor effect based on the values of delta. Herein, the effects of various input factors (according to the ranks of response tables given in Tables   5 and 6) in sequence of their effect on Ra are servo voltage U, feed rate S, pulse on time T on , and ushing pressure p. This means that ushing pressure p affects the Ra at lowest level, however, servo voltage U affects it at highest level. Hereafter, analysis of variance (ANOVA) is performed to assess the contribution of different input factors (U, T on , S, and P) on response variable Ra. Table 7 shows the analysis results by ANOVA which approves that machining voltage U, injection pressure p, wire feed rate S and pulse on time T on are signi cant machining settings for surface roughness Ra because their P-value is less than 0.05. Larger F-Value signi es that the variation of the machining setting (U, S, T on and P) results in a signi cant variation in the machining characteristics (Ra).
According to F test analysis, it can be con rmed that the highly signi cant parameters in deceasing order in terms of the effect on surface roughness (Ra) are servo voltage U, feed rate S, pulse on time T on and ushing pressure p. However, the percent contributions of the machining parameters on Ra are shown in table 7 and gure 6. Startup voltage U is found to be major factor affecting the Ra (62.94%), the percent contribution of feed rate S, pulse on time T on , and ushing pressure p on the Ra are 20.84%, 11.46%, and 4.74% respectively.  Figure 7 are presented the residual plots for surface roughness (Ra) using 18 experimental runs. We realized 9 experiments, but the roughness is tested twice for each experiment. The graphs of gure 7 demonstrates that residues found are independent while displaying a randomized dispersion. Moreover, Figure 7 shows that the variable follows the normal distribution, and the residuals are distributed roughly in a straight line, displaying a good relationship between the analytically predicted values for all Ra performances and experiment. The results presented in Table 8 are obtained with Minitab Software using ANOVA analysis. The percentage of variation in the response displayed in Table 8 is very high (R-sq(adj) >99%), thereby, the model ts well the data. The quadratic model proposed to predict surface roughness (Ra) can be expressed based on response surface analysis (RSA) as a function of U, T on , S and P in regression Equation (2)  respectively. It's clear that the dark blue zone of each graph represents the optimal cutting parameters ensuring a good surface nish quality. Figure 9-a shows that the increase in ushing pressure had not signi cant effect on surface roughness for minimal feed rate values. However, when ushing pressure converges to 80 bar, the excessive increase in feed rate S results in the highest surface roughness. Once more, if this critical value of ushing pressure is reached for lower values of pulse on time, the surface nish quality decreases signi cantly (Figure 9-b). Figure 9-c indicates that the excessive increase in servo voltage U results in a bad surface nish quality practically regardless the amount of ushing pressure p (for p less than 96 bar). But, for extreme values of servo voltage U, surface roughness reaches its maximum again when ushing pressure converges to 80 bar.
Hence, it can be concluded that to obtain good surface nish the value 80 bar of ushing pressure should be avoided for highest amounts of servo voltage U and feed rate S along with for lower levels of pulse on time T on . In fact, this nding could be supported by Figure 4-d which demonstrates that the mean S/N ratio goes down and achieves a minimum at the ushing pressure of 80 bar. However, at the same level of ushing pressure, surface roughness mean was the highest predicted as given in Figure 5-d.
Moreover, it can be observed from Figures 9-d and 9-e that a very poor surface roughness is highly expected with excessive decrease in pulse on time T on if attended by an important increase in each of servo voltage and feed rate. Finally, Figure 9-f demonstrates that the extreme surface roughness or rougher machined surface are obtained for a greater feed rate S and a higher servo voltage U.

4-1-SEM examination of white layer
Service lifetime of a wire EDMed component depends chie y on surface integrity. The latter is characterized by the microstructural alterations on the machined surface and sublayers regions (the presence of white layer), surface roughness, surface damage formation, hardness distribution, residual stresses, etc. However, the low thermal conductivity that characterizes titanium alloys makes it crucial to study the effect of the WEDM process and the machining parameters that in uence it on surface integrity, in particular surface roughness and crack formation, as reported by [16] in the EDM of the titanium alloy Ti6Al4V. The surface roughness in EDM has been de ned in [16] as a process of chip forming which takes place on surface of wire EDMed component and manifested by the presence of spherical debris particles. It has been also reported in the same investigation that crater size along with machining-induced cracks could be important factors on which the roughness of the machined surface depends. Hereafter, type of surface integrity of Ti-6242 wire EDMed samples is analyzed using SEM micrograph. The aim was to assess the effect of machining parameters on surface characteristics such as white layer thickness and surface damage density. The combinations set studied below are taken from Table 4 and completed with further cutting experiments so that the ushing pressure is xed at 100 bar. Cross sectional microstructure of the machined surface of Ti-6242 titanium alloy observed under SEM for two different sets of machining parameters is given in Figure 10. The latter shows signs typical of the material that has experienced important metallurgical alterations as it was entirely melted and was then cooled down rapidly during processing by WEDM. Figure 10 shows the presence of a recast layer (white layer), characterized by hexagonal martensitic structure in WEDM of Ti-6242 super alloy, as a result of re-solidi cation of molten metal residual portion that had not ushed away by dielectric liquid and had not experienced any hydrodynamic effect during bubble collapsing phase. Moreover, it is evident that the machined surface is covered with a white layer of varying thickness and contains microcracks and pores. Figure 10 also shows that tempered layer formed by the sublayers that have not melted by the heat produced during WEDM processing is characterized by important microstructural alterations. In fact, tempered layer is composed by larger and elongated grains as indicated in Figure 10 a and b. Coarser grain size is the result of recrystallization process at elevated temperatures inside a slight tempered layer that the thickness is of about 15µm and does not exceed 10µm for the sets 1 and 2 of machining parameters as given in Figures 10 a and b, respectively. A slight tempered layer in WEDM of Ti-6242 super alloy is well expected due to the low thermal conductivity of titanium alloys. Material microstructure of the region located below tempered layer remains unaffected by heat generated during WEDM process. This region preserves small grains size character and is considered part of base material. However, the thickness of white layer and the surface cracking generation are highly in uenced by machining parameters. Figure 10 shows that the increase in servo-voltage from 80 to 120V and the decrease in pulse on time from 1 to 0.8 µs result in a thinner white layer as the thickness of that layer has decreased from 27 to 10 µm. Indeed, the decrease in pulse on time results in a decrease in MRR because spark intensity is low, and due to low material conductivity, the amount of material removed from the machined surface is less, resulting in a small amount of resolidi ed material and a thin recast layer. Moreover, set 2 of machining parameters is characterized by a high ushing pressure, which also could lead to a thin white layer. Figure 10 shows that surface microcracks extend arbitrarily to various depths and majority of observed microcracks are found to grow towards the bulk material. Indeed, the state of residual stresses built-up within the machined surface is governed by plane tensile stresses that accumulate parallel to surface and result in microcracks normal to white layer of hard hexagonal martensitic structure. Majority of microcracks in the white layer developed using set 1 of machining parameters are deep and penetrate into the tempered layer. However, the decrease in pulse on time leads to the generation of shallow microcracks in machined surface. It can be seen also from Figure 10 that higher the pulse on time thicker the white layer, and wider and deeper the microcracks inside the machined surface. The reverse is also true.

4-2-SEM examination of machining-induced damage
SEM examination of machined surface topography has been carried out for wire EDM of Ti-6242 super alloy with respect to various combination sets of machining parameters (V, S, T on , p) taken from Table 3. Figures 11 and 12 (a, b,  of Ti-6242 super alloy in WEDM process. Each combination set is associated with the corresponding machined surface SEM micrograph via Table 9. Figure 11 shows a typical SEM micrograph of wire EDMed surface produced by the combination set 1 of machining parameters: highest levels of servo-volatge and pulse on time, medium levels of feed rate and ushing pressure according to Table 3. From SEM micrograph of Figure 11, it is obvious that machined surface reveals porous and foamy structure caused by dynamic gas bubble formation during machining. It can be also seen from Figure 11 that the machined surface is made up of droplet shaped resolidi ed material with randomly distribution of many spark-induced craters with varying size, many spherical debris, huge number of microvoids and pockmarks, and marked by the presence of surface microcracks network to form a rough surface. The effect of wire EDM cutting parameters on surface damage characteristics could be explained based on the comparison of Figures 12 (a, b, c, d) in terms of the density and widens of surface microcracks along with craters size and microvoids density. The results of such a comparison are reported in Table 10.   Figures 12 a and b). On the other hand, for a high xed feed rate (43mm/min), microcracks have been shown to be denser but narrower with the increase in pulse on time and reduction in servo-voltage (Figures 12 d and c). Moreover, at a high xed level of servo-voltage, microcracks are getting wider with the large increase in feed rate (Figures 12 b and d). At the same pulse on time, the excessive increase in feed rate S up to 43mm/min results in an increase in crater size and microvoids density. In addition, such cutting conditions have made of shallow and sub microcracks deeper, denser and wider rendering machined surface roughness more pronounced (Figures b and c). It can be also deduced from Table 10 that pulse on time has a signi cant effect on surface cracking density in accordance with the observations reported in [16]. By decreasing in pulse on time from 1 to 0.8 µs and keeping servo-voltage constant at 120V, the density of surface microcracks decreases signi cantly (Figures 12 a and d).
In Figure 13 is illustrated a histogram in which the variation of surface damage with machining parameters is quanti ed in terms of surface microcracks density (η). In Figure 13 a fth combination set of machining parameters has been included. Graph of gure 13 (combination sets 1 and 3) shows that for high feed rate and servo-voltage levels, surface cracks densities are high (η= 13.8 and 36.2 µm/µm 2 ) for relatively high levels of pulse on time T on . However, set combination 4 proves that the excessive increase in servo-voltage and feed rate cannot cause high microcracks density unless a high pulse on time is applied to cutting process. Hence, it can be concluded that for high servo-voltage and feed rate levels, pulse on time plays a critical role in promoting or inhibiting surface microcracks formation and could control surface microcracks density.
On the other hand, Figure 13 indicates that servo voltage does not exhibit an interpretable effect on surface cracking density for the levels of voltage ranging between 100 and 120V. However, it has been found that further decrease in servo-voltage to 80V is marked by a signi cant decrease in surface microcracks density (η= 1.8 µm/µm 2 ) even for high levels of feed rate and pulse on time as demonstrated in combination set 5 of Figure 13. This result could be supported by the SEM micrograph of Figure 14.

Conclusion
The investigation of nal surface quality in wire EDM of Ti-6242 titanium alloy using a brass tool electrode and deionized water as a dielectric uid has been subject of the present work. The effect of WEDM process settings such as pulse on time (T on ), servo voltage (U), feed rate (S) and ushing pressure (p) on surface roughness (Ra) has been studied. Optimization of the implicated cutting parameters for surface quality improvement has been carried out based on Taguchi's signal-to-noise ratio (S/N) approach. Accordingly, L9 (3^4) orthogonal array-based experimentation was designed, and Lower-The-Better (LTB) criteria was applied. Percent contributions of each machining parameter on SR (Ra) has been determined using ANOVA analysis, and a quadratic model expressed with U, T on , S and P to predict SR (Ra) has been established using response surface analysis (RSA). SEM observations were performed to examine microstructural alterations and machining-induced surface-breaking cracks in wire EDMed surface of Ti-6242 super alloy. The effect of the involved machining parameters on white layer thickness and surface microcracks density has been discussed deeply. During this investigation it was established that: The lowest surface roughness (Ra) is achieved at the values 100 V, 0.9 µs, 29 mm/min and 60 bar for U, T on , S and p, respectively.
Startup voltage U was found to be the most important factor affecting the SR (Ra) with percent contribution of 62.94%. The percent contribution of feed rate S, pulse on time T on , and ushing pressure p on Ra are 20.84%, 11.46%, and 4.74% respectively.
The predictive model of surface roughness is quite accurate and could be explored to forecast (Ra) in wire EDM of Ti-6242 titanium alloy.
Contours plots revealed that the rougher Ti-6242 surface is obtained at high levels of servo-voltage U and feed rate S for critical ushing pressure p close to 80 bar.
SEM examination of machined surface demonstrated that white layer thickness and surface damage characteristics are highly dependent on cutting parameters.
Even though there was great growth in servo-voltage V, the large decrease in pulse on time T on results in a decrease in white layer thickness with the generation of shallow microcracks.
The decrease in pulse on time T on and feed rate S results in a large decrease in overall machining-induced damage at high servovoltage V.
Surface microcracks are getting wider (at a high xed level of servo-voltage V) with the large increase in feed rate S.
Pulse duration T on plays a role of regulating the surface microcracks density at high servo-voltage V and feed rate S levels.
The lower surface microcracks density is achieved for lower servo-voltage V even though pulse on time T on and feed rate S are extreme.  Surface integrity assessment strategy pursued in present work   Main Effects plot for means on surface roughness Ra Figure 6 Percentage contribution of control factors for Ra.

Figure 8
Comparison between measured and predicted values for Ra.

Figure 9
Contour plots of surface roughness Ra. Variation of surface cracks density η (µm/µm2) with cutting conditions Figure 14