Evergreen — Joint Journal of Novel Carbon Resource Sciences and Green Asia Strategy
Article Open Access CC BY 4.0 Vol 13 · Iss 02 · June 2026 · pp. 629–642

Optimization of Stir-Cast AA6063 Hybrid Composites Reinforced with Rice Husk Ash and Marble Dust Using Taguchi-Grey Relational Analysis

Prashant Kumar1, Dheeraj Joshi1, Bhavana Mathur2

1 Department of Mechanical Engineering, Swami Keshvanand Institute of Technology, Management & Gramothan, Jaipur 302017, India
2 Department of Mechanical Engineering, Anand International College of Engineering, Jaipur 302012, India

Corresponding author: kprashant709@gmail.com  ·  Prashant Kumar

ReceivedApril 28, 2025
AcceptedApril 19, 2026
PublishedJune 2026

Abstract

Hybrid aluminium matrix composites (HAMCs) have emerged as promising materials owing to their superior mechanical and tribological performance. In the present study, AA6063-based HAMCs were developed using 5 wt.% silicon carbide (SiC) and 5 wt.% graphite (Gr) as primary reinforcements, along with 1.5–2.5 wt.% rice husk ash (RHA) and marble dust (MD) as secondary reinforcements. The composites were fabricated via stir casting based on a Taguchi L16 orthogonal array, considering pouring temperature (PT) and stirring speed (SS), wt.% RHA and wt.% MD as process parameters. Mechanical and tribological properties, including tensile strength, microhardness, wear rate, and density, were evaluated. Multi-response optimization was carried out using Grey Relational Analysis (GRA), wherein grey relational grades (GRG) were computed and ranked to determine the optimal experimental conditions. Further, analysis of variance (ANOVA) was performed on GRG to identify the significance and contribution of process parameters. The results demonstrate the effectiveness of the integrated Taguchi–GRA approach in determining optimal processing conditions for AA6063 hybrid composites.

Keywords: ANOVA, Density, Grey relational analysis, Microhardness, Porosity, Stir casting, Tensile Strength, Wear rate

Outline

1. Introduction

Hybrid aluminium Matrix Composites (HAMCs), which combine two or more reinforcements, have emerged as a promising approach to achieve the desired properties of AMCs. In recent years, agricultural and industrial waste-derived reinforcements have emerged as sustainable, low-cost alternatives for enhancing aluminium metal matrix composites (AMMCs), offering environmental benefits alongside improved mechanical and tribological performance1,2). Diverse agro-wastes and industrial waste are being used by various researchers, such as ground nut shell ash3), coconut shell ash4,5), fly ash6-8),, snail shell ash9), plantain peel ash10), corn cob ash11), palm kernel shell12), ash, neem leaf ash13), straw ash14,15), etc have been effectively incorporated into aluminium matrices to boost properties like hardness, strength, and wear. Traditional ceramic reinforcements such as silicon carbide (SiC)16-18) and graphite (Gr)19-21) have been extensively used to enhance hardness and wear resistance and to provide self-lubricating characteristics in aluminum alloys. Recent studies indicate that combining these conventional ceramics with agro-waste or industrial by-products produces composites with customized properties, offering a balance of cost efficiency, environmental sustainability, and improved mechanical performance. The use of Silicon Carbide (SiC) and Graphite (Gr) as primary reinforcements is common, as they offer excellent mechanical properties. However, the addition of secondary reinforcements, such as Rice Husk Ash (RHA) and Marble Dust, presents a more sustainable and cost-effective solution. These materials, often considered waste products, offer environmental benefits by reducing waste while enhancing the properties of the composite. Rice Husk Ash contains more silica and contributes to improved wear resistance and hardness. Many researchers have used RHA for their study22-24). On the other hand, marble dust (MD), a waste material generated from the stone-cutting industry, primarily consists of calcium carbonate along with some silica, making it an economical option for reinforcing materials to improve hardness and wear resistance. Many researchers have also used MD in their research work25,26).

Despite the numerous benefits, the creation of hybrid composites necessitates the optimization of processing parameters in order to obtain the necessary material performance. Pouring temperature, stirring speed, and stirring duration are important process parameters that influence the microstructure and, consequently, the composite's properties. Therefore, it is crucial to identify the optimal processing conditions.

When working with multiple responses, Grey Relational Analysis (GRA) techniques hold a great interest for the researchers, especially for their use in Taguchi-based GRA. This statistical approach effectively determines optimal process parameters by simultaneously evaluating multiple performance characteristics, making it a powerful tool for addressing complex optimization problems. Several research studies have demonstrated the effectiveness of GRA in various applications, for example, H. S. Jailani et al.27), focused on how to improve the combination of sintering process parameters of Al-Si alloy reinforced with fly ash composites by applying Taguchi-GRA in a powder metallurgy technique. The investigation changed the fly ash concentration from 5 wt.to 15wt.%, also the compacting pressure was changed from 307-512 MPa, finally, the sintering temperature parameter also changed from 575-625°C. Analyzing their influence on density and hardness. GRA optimization successfully identified the optimal process settings, confirming that sintering parameters significantly influence mechanical properties.

Similarly, in another work by S. Dharmalingam et al.28), the application of Taguchi-GRA optimization was seen to improve the wear resistance in aluminium hybrid composites utilizing the alumina (Al₂O₃) and molybdenum disulfide as reinforcements. In this study, for designing the experiments, Taguchi L-9 orthogonal array was utilized, and process parameters like applied load, sliding speed, abrasive size, and MoS₂ content were optimized to get the improved wear resistance of the composite, validating GRA's efficacy in hybrid composite research.

The application of Taguchi-GRA methodology for improving the machining process was seen in the study done by P. Jayaraman et al.,29). Different machining parameters like cutting speed, feed rate, and depth of cut were consider to study their impact on the surface roughness of the component also focusing on material removal rate. This study also supported the role of Taguchi-GRA technique to improves machining performance by lowering surface roughness and increasing material removal efficiency.

Similarly, A.K. Mishra et al.30), focused on improving the wear resistance in their work. Here AA6061 alloy was consider for study with SiC (15 wt.%) and Al₂O₃ (15 wt.%) as reinforcements. For designing the experiments Taguchi L-27 orthogonal array was applied. Their dry sliding wear studies on a pin-on-disc apparatus revealed that sliding distance was critical for controlling friction and wear. Furthermore, optical microscopy of wear tracks revealed insights into the wear mechanisms at work. Their findings revealed that optimized hybrid composites have higher wear resistance under certain process settings.

In another work the application of Taguchi-based GRA was seen along with Principal Component Analysis as investigated by, N. Kaushik et al.31). AA6063 alloy was consider in this study. SiC was chosen as the reinforcement. The study looked at three different weight fractions of SiC reinforcements (3.5 wt.%, 7.5%, and 10.5%) to analyse how the different wt.% of reinforcements affect the properties like wear rate, specific wear rate, and frictional force. The experiments performed on a pin-on-disc tribometer showed that increasing SiC content led to significant wear resistance improvements under optimized process conditions. ANOVA results confirmed the statistical significance of control parameters, and optical microscopy of worn-out specimens revealed dominant wear mechanisms.

In another work, E.M et al.32), evaluated how Gr affects the aluminium composite with SiC as primary reinforcement. Here also the machining parameters were also studied. From the study, it was clear that the cutting speed with maximum percentage contribution of 48.76%, as found by performing ANOVA analysis found to be the most important factor that affects the responses like Surface roughness and material removal rate. After that, parameters like feed rate and depth of cut influenced the responses. Furthermore, Taguchi's predictive model was validated by comparing experimental and forecasted roughness values, demonstrating the importance of elemental chip production in lowering surface roughness.

Another key study by M.K. Rahimana et al.33), investigated the application of Grey relational analysis on friction stir welding (FSW). In this study, an attempt was made to join dissimilar aluminium alloys like AA7075 and AA6061. The parameters, like specimen thickness, axial force, and transverse speed, for studied. Tensile strength was taken as a response factor for this study. The specimens were made as per Taguchi's L9 orthogonal array for multi-response optimization, and ANOVA demonstrated that process factors significantly affected tensile strength.

Similarly, Taguchi-based Grey Relational Analysis was applied to the investigation done by S.V. Alagarsamy et al.34). In this study, AA 7075 was taken as the base alloy and TiO₂ particles with different wt.% (0, 5, 10, and 15 wt.%) as reinforcements. Here stir casting method was applied for the composite. The experiment aimed to optimize the wear performance considering the process parameters like applied load, sliding distance, reinforcement percentage, and sliding velocity. From the results, it was seen that the wear resistance was influenced by the reinforcement wt.% after the applied load. The worn-out surface was also studied through SEM micrographs. A confirmation experiment corroborated the projected ideal findings.

The application of Grey Relational Analysis (GRA) was also seen in another work based on friction stir welding done by I. Sabry et al.35), for 6061-T3 aluminium alloy flanges. The response factors, namely tensile strength, % elongation, bending load, and yield strength, were considered in this study. Welding parameters such as travel speed, rotation speed, shoulder diameter, and rotation speed at different levels were varied in this study. The application of Grey Relational Analysis (GRA) successfully optimized the welding parameters.

The hybrid metal-matrix composites prepared using powder metallurgy were investigated by B. A Gemeda et al.36). Here, Taguchi-based Grey Relational Analysis was also applied to optimize the process parameters. The composites were made using the reinforcements B4C, SiC, ZrO2, and MoS2 to study the physico-mechanical properties of hybrid composites. The parameters, namely milling duration of 5 hours, sintering temperature of 1200 °C, and finally compaction pressure of 40 MPa, lead to improvement in the properties like wear resistance, hardness, and compressive strength

The Taguchi-based GRA, a multi-objective optimization technique, has great potential to improve the efficiency and performance of a variety of processes. Given its ability to examine multiple performance factors simultaneously, it can determine optimal process parameters. The present study also focuses on how different process parameters can be optimized using Taguchi-based GRA, considering multiple responses. For the present study, AA6063 hybrid composites reinforced with fixed percentages of SiC and Gr (5 wt.%) and varying percentages of secondary reinforcements, namely RHA and Marble Dust. To find the percentage contribution of each parameter, ANOVA was performed. The optimization results are then evaluated using confirmation tests, and the composites' performance is compared to that of pure AA6063 and other single-reinforced polymers.

This study intends to contribute to the field of sustainable materials by proving the effective utilization of waste goods like rice husk ash and marble dust.in enhancing the performance of aluminum matrix composites. Furthermore, the study highlights the potential of Taguchi and GRA methods to optimize the fabrication process of hybrid composites, achieving superior properties while maintaining cost-effectiveness.

2. Materials and Methods

2.1. Matrix Selection

In the present study, AA6063 has been selected due to its light weight, ease of fabrication, and castability properties. AA6063 was purchased from Rajasthan Aluminum, Tripolia Bazar, Jaipur, Rajasthan, and its elemental content

Table 1: Chemical Composition of AA 6063 Alloy

ElementsComp. AnalyzedNominal Comp.
Si0.510.2-0.6
Fe0.15Max 0.35
Mg0.550.45-0.9
Zn0.01Max 0.1
Cu0.01Max 0.1
Mn0.04Max 0.1
Cr0.01Max 0.1
AlBalanceBalance

is presented in Table 1.

2.2. Reinforcement Selection

In the present study, SiC, Gr, Rice husk ash (RHA), and Marble dust (MD) were used as reinforcements. Incorporating soft reinforcements like graphite alongside hard ceramic particles such as SiC reduces brittleness while boosting wear resistance, ultimately improving the performance of hybrid composites37). Research has shown that adding these ceramic particulates to aluminum-based composites markedly enhances their mechanical and tribological properties. For example, B. Suresh Babu et al.38) produced AA6063 hybrid composites via stir casting, with a formulation of 90 wt.% Al, 5 wt.% SiC, and 5 wt.% graphite achieving higher tensile strength (190.48 MPa) and lower density (2.64 g/cm³) than a comparable 90 wt.% Al with 10 wt.% SiC variant (160.84 MPa, 2.71 g/cm³).In addition to these primary reinforcements, Rice Husk Ash (RHA), an environmentally acceptable substance with high silica content, and industrial waste such as marble dust are considered secondary reinforcements. contributing towards sustainability39,40). The Rice husk ash (RHA) was purchased from Herenba Instruments & Engineers, Kaveri Street, Ramnagar, Ambattur, Chennai, whose constituents are presented in Table 2.

Hybrid (three or multi-phase) composites offer greater flexibility in tailoring material properties than two-phase composites41), and are increasingly being explored in the aerospace and automotive sectors for their superior strength-to-weight ratio, reduced density, and improved ductility. Therefore, MD was included to provide increased hardness and strength, along with a cost-effective solution for composite fabrication42). The marble dust was procured from a local marble processing plant, Yogesh Moorti Kala Kendra, Jaipur. The chemical compositions of marble dust are presented in Table 3.

Table 2: Constituents of Rice Husk Ash (RHA)

Compound/element(constituent)wt.%
SiO291.56
C4.8
CaO1.58
MgO0.53
Fe2O30.21
K2O0.39
Others0.93

Table 3: Constituents of Marble Dust (MD)

Compound/element(constituent)wt.%
CaO42.45
MgO1.52
SiO226.35
Al2O30.520
Fe2O39.40

2.3. Design of Experiments

The experiments were designed according to Taguchi's L16 Orthogonal arrays. Four different process parameters were taken at four levels as shown in Table 4. The wt. % of SiC and Gr was kept constant at 5 wt. %. The pouring temperature (PT) levels were taken as 660, 680, 700, and 720 °C. A stirring time of 15 minutes was taken common for all experiments. Finally, the stirring speed (SS) was taken as 300,400,500,600 rpm. The process parameters were selected properly selected according to the literature review43-45). The experiments designed as per Taguchi's L16 Orthogonal array are shown in Table 5.

Table 4: Different levels of process parameters and their notation

Process parametersNotation.1234
Pouring Temp (PT) (°C)PT660680700720
Stirring Speed (SS) (rpm)SP300400500600
wt.% of Rice Husk Ash (RHA)RHA11.522.5
wt.% of Marble Dust (MD)MD11.522.5

Table 5: Experimental Design according to Taguchi’s L 16 orthogonal array

Exp. NoPT
(°C)
SS
(rpm)
RHA
(wt.%)
MD
(wt.%)
166030011
26604001.51.5
366050022
46606002.52.5
56803001.52
668040012.5
76805002.51
868060021.5
970030022.5
107004002.52
1170050011.5
127006001.51
137203002.51.5
1472040021
157205001.52.5
1672060012

2.4. Composite Fabrication by Stir Casting

The stir casting method for producing metal matrix composites is widely used due to its simplicity and cost-effectiveness. This method can be used to generate hybrid metal-matrix composites. Various researchers are using aluminium metal matrix composites produced by this method to improve their mechanical and wear properties46-48). This study used a bottom-tapping stir-casting furnace with a crucible that can accommodate up to 2 kg of aluminium alloy at a time. This type of machine supports a maximum temperature of 1000 °C for composite generation. The samples were prepared according to the Taguchi L-16 orthogonal array, as shown in Table 5. The reinforcements were preheated in the preheater chamber before mixing with the stirrer in the furnace. The Rectangular die was heated to 250 to 300 °C before pouring the melt. The stirring speed, pouring on/off, preheated temperature, lifting of the stirrer etc., are also controlled. At last, the die is opened to take out the cast.

2.5. Mechanical Characterization

2.5.1. Tensile testing

The tensile testing of the specimen was done on a 30KN tensile testing machine. The samples were prepared following the ASTM E8 standard, as shown in Figure1.

A gauge length of 32 mm was taken for tensile testing.

2.5.2. Micro hardness testing

The microhardness of the prepared samples was determined using a Vickers microhardness tester. Before that, the test sample of size 30mm×20mm×10mm as represented in Figure1 was mirror polished using different grades of emery papers, a disc polishing machine using aluminium paste, and finally etched with reagents (Keller's reagent). During measurement of microhardness, a constant load of 100-kgf and a dwelling time of 30 seconds was maintained for each sample.

2.5.3. Wear testing

Tribological testing employed a universal tribometer for unlubricated ball-on-flat linear reciprocating wear experiments. Test specimens measured 30 mm × 10 mm × 10 mm to assess wear resistance. Tests were conducted at ambient temperature (300 K), using a 5 mm stroke length, 20 N normal load, and 5 Hz frequency. Coefficient of friction (COF) was recorded continuously over 600 seconds of sliding. Specific wear rate (SWR) was computed using Eq. (1)49). Sample mass loss was determined via Eq. (2) and sliding distance was calculated using Eq. (3).

SWR=mρ×Sd×F (mm3/Nm)(1)
m=mi-mf (2)

ρ=Density of the composite (g/cm3)

Sd=Sliding Distance (meters)

𝑆𝑑=2×𝐿×𝑓×𝑇(3)

F=Applied Load (Newton)

Where L = stroke length (m)

f = frequency (Hz)

t = total test time (s)

The loss of mass for each sample is presented in Figure2.

Figure 1
Fig. 1: Standard samples for response measurement
Figure 2
Fig. 2: Mass loss of sixteen samples

2.5.4. Density Calculation

Using the Rule of Mixtures, the theoretical density of the composites was obtained by Eq. (4)18). AA6063 alloy, silicon carbide (SiC), graphite (Gr), rice husk ash (RHA), and marble dust (MD) are represented by the weight percentages WAl6063, WSiC, WGr, WRHA, and WMD in this equation, respectively. The corresponding densities of Al6063, silicon carbide, graphite, rice husk ash, and marble dust are denoted by ρAl-6063, ρSiC, ρGr, ρRHA, and ρMD, and their assumed values as per literatures are shown in Table 6. To calculate density experimentally, the mass of each sample was divided by its volume.

ρT=1WAl6063 ρAl6063+WSiC ρSiC+WGr ρGr+WRHA ρRHA+WMD ρMD (4)

The measured theoretical and experimental densities were compared using Eq. (5) to determine the composites' % porosity50).

% P=pT-pExpT×100 (5)

Where pT is the density obtained theoretically

pEx is the density obtained experimentally

Table 6: Densities of Constituent Elements for Theoretical Density Estimation13,18,22,51)

ElementDensity
ρ(g/cm3)
Al60632.7
Gr2.23
SiC3.21
RHA1.60
MD2.68

2.6. Multi-Response Optimization Steps in GRA

The multi-response optimization problem considered in the present study was addressed using Grey Relational Analysis (GRA), a widely used technique for solving multi-attribute decision-making problems. GRA is based on the evaluation of the degree of correlation between sequences and is particularly suitable for systems with incomplete or uncertain information. The method transforms multiple performance characteristics into a single representative index, known as the grey relational grade (GRG)52), which reflects the overall performance of the system.

In the present work, the experimental responses, namely ultimate tensile strength, microhardness, wear rate, and density, were first normalized to eliminate the effects of different units and scales. For the responses where higher values are desirable, such as tensile strength and hardness, the normalization was carried out using equation (6), whereas for responses where lower values are preferred, such as wear rate, the normalization was performed using equation (7).

yi(k)=xi(k)-minxi(k)maxxi(k)-minxi(k)(6)
yi(k)=maxxi(k)-xi(k)maxxi(k)-minxi(k)(7)

After calculating the Normalized value for each tensile and micro hardness, wear, and density, the deviation was calculated using equation (8).

i(k)=||maxyi(k)-yi(k)||(8)

The computed deviation is displayed in Table 12. Equation (9) was then used to determine the grey relationship coefficient.

ξi(k)=min Δi(k)+ψ𝑚𝑎𝑥 Δi(k) Δi(k)+ψ𝑚𝑎𝑥 Δi(k)(9)

Where0ψ0.5

Table 13 presents the calculated Grey relational coefficient. Equation (10) was used for calculating grey relational grades.

γ=1nk=1nξi(k)(10)

The rank is presented in Table 13.

Equation (11) was used for calculating the predicted value of grey relational grades.

γpredicted=γn+i=1q(γ¯-γn)(11)

Where q represents the number of significant input parameters, also  γ¯ represents the mean value of GRGs. Additionally,  γ¯ denotes the means of GRGs while considering the optimal level. The number of responses is denoted by n.

3. Results and Discussion

3.1. Mechanical Characterization

The mechanical and tribological properties of the developed AA6063 hybrid composites were evaluated in terms of ultimate tensile strength (UTS), microhardness (HV), wear rate, and density, and the results are presented in Table 7. The UTS values were found to vary from 136.98 MPa to 151.11 MPa, with the maximum value obtained for Experiment 13 (PT = 720°C), indicating the positive influence of higher processing temperature and optimized reinforcement composition on load-bearing capacity. Similarly, the hardness values ranged from 69.76 HV to 81.42 HV, with the highest hardness observed in Experiment 14, attributed to the uniform distribution of hard reinforcement particles and improved interfacial bonding. The wear rate exhibited a decreasing trend with increasing reinforcement and temperature, ranging from 0.0082 mm³/Nm to 0.0055 mm³/Nm, indicating enhanced wear resistance due to the presence of hard ceramic phases and improved surface integrity. Theoretical density (ρT)and experimental density (ρEx)values were found to be in close agreement, with porosity values remaining below ~1.55% for most samples. However, slightly higher porosity was observed in certain cases (e.g., Experiments 7 and 14), which may be attributed to improper wetting or gas entrapment during casting.

3.2. Grey Relational Analysis

The signal-to-noise (S/N) ratios were calculated using the “larger-the-better” criterion for UTS and HV, and the “smaller-the-better” criterion for SWR and density, as given in Table 8. The computed S/N ratios are listed in Table 9. To eliminate unit variations, the S/N ratios were normalized using Eqs. (1) and (2), and the normalized values are presented in Table 10. The deviation sequences were then calculated using Eq. (3), and the results are shown in Table 11. Based on these deviations, the grey relational coefficients (GRCs) were determined using Eq. (4).

The grey relational grades (GRGs), representing the overall performance index, were calculated using Eq. (5) and are presented in Table 12 along with their ranks. Among all experiments, Experiment 12 exhibited the highest GRG (0.7217), indicating the best combination of process parameters for achieving optimal mechanical and tribological properties.

Table 7: Experimental Results of Mechanical and Tribological Properties

Ex. noPT
(°C)
SS (rpm)RHA
(wt.%)
MD
(wt.%)
UTS
(MPa)
HVSWR (mm3/Nm)ρ𝑻 (g/cm3)ρ𝑬𝒙 (g/cm3)% P
166030011136.987069.76830.00822.67452.66350.4112
26604001.51.5139.986570.90930.00802.66532.66270.0975
366050022138.204972.13000.00722.65622.65130.1844
46606002.52.5142.662173.37940.00702.64712.64530.0679
56803001.52140.280071.42620.00792.65612.65330.1054
668040012.5137.154870.33220.00812.64732.64480.0944
76805002.51144.107374.56330.00642.67382.63281.5333
868060021.5143.169676.25090.00662.66642.64310.8738
970030022.5146.747675.73150.00682.65162.64870.1093
107004002.52148.718677.12250.00562.65642.63120.9486
1170050011.5145.415875.82580.00692.66752.65630.4198
127006001.51149.110378.63060.00632.67482.66320.4336
137203002.51.5151.116579.48980.00612.66662.63411.2187
1472040021150.126381.42200.00552.67492.63351.5477
157205001.52.5148.415679.27250.00632.64742.64560.0679
1672060012149.022278.67520.00562.65602.64490.4179

Table 8: Signal-to-noise ratio (ɳ) functions for desired Goals

S/N functionS/N formulaGoal
Smaller the betterSN=-10log[13i=1i=nyi2]Min:𝒑𝑬𝒙
Minimizing: SWR
Larger the betterSN=-10log[1ni=1i=n1yi2]Maximizing: UTS
Maximizing: HV

Table 9: Calculated Signal-to-Noise (S/N) Ratios for Experimental Responses

Criteria (The larger is the better)Criteria (The smaller the better)
Ex. noUTS
(MPa)
HV𝒑𝑬𝒙
(g/cm3)
SWR
142.733636.8732-8.509141.7237
242.921737.0141-8.506441.9382
342.810537.1623-8.469242.8533
443.086237.3115-8.449543.0980
542.939937.0772-8.475742.0474
642.744236.9431-8.447941.8303
743.173737.4505-8.408443.8764
843.117037.6449-8.442343.6091
943.331437.5855-8.460743.3498
1043.447337.7436-8.403145.0362
1143.252237.5963-8.485543.2230
1243.470237.9118-8.508144.0131
1343.586238.0062-8.412644.2934
1443.529138.2148-8.410745.1927
1543.429637.9825-8.450544.0131
1643.465037.9168-8.448245.0362
Max43.586238.2148-8.403145.1927
Min42.733636.8732-8.509141.7237

Table 10: Normalized Signal-to-Noise (S/N) Ratios for Experimental Responses

Criteria (The larger is the better)Criteria (The smaller the better)
Ex. noUTS
(MPa)
HVSWR
(mm3/Nm)
ρ𝑬𝒙
(g/cm3)
10.00000.00001.00000.5512
20.22060.10500.93820.5250
30.09010.21550.67440.4027
40.41350.32670.60380.0000
50.24200.15200.90670.3634
60.01250.05210.96930.0131
70.51610.43030.37940.4201
80.44960.57520.45650.8433
90.70110.53090.53120.2584
100.83700.64870.04510.5118
110.60820.53900.56781.0000
120.86380.77410.34000.6079
131.00000.84450.25920.9651
140.93301.00000.00000.7561
150.81620.82680.34000.1533
160.85780.77780.04510.5076
Min0.00000.00000.00000.0000
Max1.00001.00001.00001.0000

Table 11: Deviation Sequences for Normalized Responses

Criteria (The larger is the better)Criteria (The smaller the better)
Ex. noUTS
(MPa)
HVSWR
(mm3/Nm)
ρ𝑬𝒙 
(g/cm3)
10.00000.00001.00000.5512
20.22060.10500.93820.5250
30.09010.21550.67440.4027
40.41350.32670.60380.0000
50.24200.15200.90670.3634
60.01250.05210.96930.0131
70.51610.43030.37940.4201
80.44960.57520.45650.8433
90.70110.53090.53120.2584
100.83700.64870.04510.5118
110.60820.53900.56781.0000
120.86380.77410.34000.6079
131.00000.84450.25920.9651
140.93301.00000.00000.7561
150.81620.82680.34000.1533
160.85780.77780.04510.5076
Min0.00000.00000.00000.0000
Max1.00001.00001.00001.0000

Table 12: Grey Relational Coefficients (GRCs), Grey Relational Grades (GRGs), and Ranking of Experiments

Grey Relational Coefficients
Ex. noUTS
(MPa)
HVSWR
(mm3/Nm)
ρ𝑬𝒙
(g/cm3)
GRGsRank
10.33330.33331.00001.00000.66672
20.39080.35840.88990.95230.64793
30.35460.38920.60560.57040.480014
40.46010.42610.55790.47070.478715
50.39740.37090.84270.61360.55629
60.33610.34530.94210.46390.521911
70.50820.46740.44620.34470.441616
80.47600.54060.47920.44230.484513
90.62580.51590.51610.52250.545110
100.75410.58730.34370.33330.504612
110.56060.52020.53640.69230.57747
120.78590.68880.43100.98100.72171
131.00000.76270.40300.35460.63015
140.88170.99990.33330.35000.64124
150.73120.7426670.43100.47480.59496
160.77850.6923220.34370.46530.56998

4. ANOVA and Optimization of Grey Relational Grade

ANOVA was performed, taking the GRG value as the response. It was done to find out the significance and contribution of each parameter in improving the response variables. The ANOVA results are presented in Table 14. Table 14 shows the F-ratio value and P-values from the ANOVA calculation. From Table 14, it was shown that the RHA and PT significantly affected the GRG values, followed by MD and SP.

The percentage contribution of each process parameter is presented in Figure4, which clearly states that the RHA wt.% has the maximum contribution of 33.49% in increasing the GRG value, followed by pouring temp with 27.41 % contribution, followed by Marble dust 22.95% contribution, and lastly Stirring speed with 13.04% contribution.

As indicated in Table 16, the confirmatory test was also conducted. The main effect plot for average grey relational grades, as presented in Figure3, clearly states the optimal levels of process parameters. Table 13 presents the maximum values of the different process parameters at different levels. These values are marked in bold (Asterix). From Table 13, it was clear that the RHA wt.%, which has the rank 1, affects the response factors more, followed by Pouring temp assigned rank 2, Marble dust wt.% assigned rank 3, and finally the stirring speed assigned rank 4. The major effect plot for average GRGs, as displayed in Figure 3, determines the optimal values of the process parameters. From Figure3, the optimized values are pouring temp of 720, stirring speed of 300 rpm, RHA wt.% of 1.5, and MD wt.% of 1%.

Table 13: Response table showing average grey relational grades

Average grey relational grade based on factor levels (AGV)
Control Factors1234Max-Min (Ei)Rank
PT0.56830.50110.58720.6091*0.10802
SP0.5995*0.57890.52350.56370.07604
RHA0.58400.6302*0.53770.51380.11641
MD0.6178*0.58500.52770.53520.09013
Figure 3
Fig. 3: Main effect plot for AVG GRGs

Table 14: ANOVA table for average grey relational grade

Analysis of Variance
SourceDFAdj SSAdj MSF-ValueP-Value
PT30.0260950.0086988.800.050
SP30.0124130.0041384.190.135
RHA30.0318870.01062910.750.041
MD30.0218530.0072847.370.068
Error30.0029660.000989
Total150.095215
Figure 4
Fig. 4: % Contribution of individual parameters on GRG

5. Confirmation Experiments

The purpose of the confirmation test was to evaluate the analysis's efficacy. The ideal set of parameters,as shown in Table 15 was used to prepare a optimized sample (OS), as indicated in Tables 16. From the analysis, it was found that the optimized sample (OS) showed increased tensile strength as compared to sixteen samples, as shown in Figure5(a). Similarly, it showed increased microhardness as compared to sixteen samples, as shown in Figure5(b). Also, it showed reduced wear as compared to sixteen samples, as shown in Figure5(c), and finally, it showed reduced density as compared to sixteen samples, as shown in Figure5(d).

5.1. Interaction Plot

The interaction plot for Grey Relational Grades (GRGs) as shown in Figure6 shows significant interactions among the process parameters: Processing Temperature (PT), a process parameter (SP), Rice Husk Ash (RHA), and another process variable (MD). It is clear from the non-parallel and intersecting lines that the one parameter varies with changes in another showing interaction between them. Notable interactions are observed between PT and RHA, as well as between SP and MD, where the trends show considerable variations. The GRG values fluctuate across different levels of parameters, indicating their combined influence on the response.

Table 15: Optimal parameter setting for the hybrid metal matrix composites

PTSSRHAMD
720֯ C300 RPM1.5 wt.%1 wt.%

Table 16: Confirmation test results

SampleUTS
(MPa)
HVρ𝑬𝒙
(g/cm3)
SWR
(mm3/Nm)
OS154.327082.41562.63090.0053

Fig. 5(a): Tensile strength of samples including optimized sample (OS)

Fig. 5(b): Microhardness of samples including optimized sample (OS)

Fig. 5(c): Specific wear rate of samples including the optimized sample (OS)

Fig. 5(d): Experimental density of samples including optimized sample (OS)

Figure 5
Fig. 6: Interaction Plot for GRG

6. Conclusions

The present study on the multi-response optimization of AA6063 hybrid composites using the Taguchi–Grey Relational Analysis approach leads to the following conclusions:

Grey Relational Analysis effectively converted the multi-response problem into a single performance index, enabling simultaneous optimization of mechanical and tribological properties.

The optimal combination of process parameters was identified as pouring temperature of 720°C, stirring speed of 300 rpm, RHA content of 1.5 wt.%, and marble dust content of 1 wt.%, yielding the highest overall performance.

The developed composites exhibited improved tensile strength, hardness, and wear resistance under optimized conditions, demonstrating the effectiveness of hybrid reinforcement.

ANOVA results revealed that RHA wt.% is the most significant parameter with a contribution of 33.49%, followed by processing temperature (27.41%), marble dust (22.95%), and stirring speed (13.04%).

The relatively low error variance indicates good experimental reliability and consistency of results.

The confirmation test results showed close agreement with predicted values, validating the effectiveness of the Taguchi–GRA methodology.

The optimized parameters from Taguchi-based grey relational analysis were successfully identified.

The interaction plot for Grey Relational Grades (GRGs) shows significant interactions among the process parameters.

Acknowledgements

I express my sincere gratitude to Swami Keshvanand Institute of Technology, Management & Gramothan, Jaipur, and Anand International College of Engineering, Jaipur, for their invaluable support and research facilities that contributed to the successful completion of this study. I am also thankful to IIT (ISM) Dhanbad for providing access to advanced laboratory facilities and assistance in conducting the experimental investigations.

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