Open Access Article
Radha Krishna Gopidesi*a,
Kautkar Nitin Uttamraob,
Channa Keshava Naik N.
*c,
Premkartikkumar S Rd,
Ahmed Adnan Hadie,
K. Sunil Kumarf,
T. M. Yunus Khan
g,
Abdul Saddique Shaikg and
Ahmed A. Alamiery
h
aSchool of Engineering, Department of Mechanical Engineering, Presidency University, Bengalore, India. E-mail: gopidesi.radhakrishna@presidencyuniversity.in
bSVERI's College of Engineering, Pandharpur 413304, Maharashtra, India. E-mail: nitin.kautkar@gmail.com
cDepartment of Mechanical Engineering, BGS College of Engineering and Technology, Bangalore 560086, Karnataka, India. E-mail: naikphd.sit@gmail.com
dDepartment of Automotive Engineering, SMEC, Vellore Institute of Technology (VIT), Vellore, India. E-mail: premgreentech46@gmail.com
eArtificial Intelligence Sciences Department, College of Sciences, Al-Mustaqbal University, 51001, Babil, Iraq. E-mail: ahmed.adnan@uomus.edu.iq
fDepartment of Marine Engineering, Faculty of Engineering, Sri Venkateswara College of Engineering, Pennalur, Chennai 602117, India. E-mail: sunilkumarkresearcher@gmail.com
gDepartment of Mechanical Engineering, College of Engineering, King Khalid University, Abha 61421, Saudi Arabia. E-mail: yunus.tatagar@gmail.com; ashaik@kku.edu.sa
hAl-Ayen Scientific Research Center, Al-Ayen Iraqi University, AUIQ, An Nasiriyah, P.O. Box: 64004, Thi Qar, Iraq. E-mail: dr.ahmed1975@gmail.com
First published on 19th December 2025
This research explores the influence of different compression ratios (CRs) on the performance and emission properties of a fly ash-coated low heat rejection (LHR) diesel engine operated with a nano-Al2O3-based emulsified cotton seed biodiesel blend (B20W10Al200). An extensive experimental design was implemented based on the history data-based response surface methodology (RSM), taking brake power (BP) and CR as significant variables. Engine responses like brake thermal efficiency (BTE), brake specific fuel consumption (BSFC), and significant exhaust emissions (NOx, HC, CO, and smoke opacity) were examined over CR values of 16, 17, and 18. The findings identified CR18 as the best configuration, where the maximum BTE (29.03%) and minimum BSFC (0.269 kg kW−1 h−1) were obtained. A notable decrease in emissions was seen, most notably in CO (0.104%) and smoke opacity (19.3%), with NOx emissions significantly lower for CR16. To improve the predictive performance and facilitate optimization, machine learning methods were incorporated. Extreme gradient boosting (XGBoost) models performed efficiently, with R2 values greater than 0.90 for all the parameters. SHapley additive exPlanations (SHAP) revealed that brake power is the dominant control factor influencing the prediction of the response variable. Multi-response desirability-based optimization, performed through the Design-Expert software, indicated an optimum setup (maximize BTE/minimize BSFC and smoke while controlling NOx) at BP = 2.49 kW and CR = 18, which had a composite desirability value of 0.751. This study confirms the combined potential of thermal barrier-coated LHR engines and nano-emulsified biofuels under optimal conditions, validating the shift toward cleaner and more efficient combustion in compression ignition engines.
Among the available options, nanoparticle additives are also the most favorable fuel catalysts, which help to shorten the evaporation and ignition delay time at the same time. The foremost requirement of nanoparticles is listed below. Overall, the interference of nanoparticles in fuel ultimately leads to enhanced oxidation power to improve rapid fuel combustion. They should maintain the conventional engine working operation throughout their involvement. Although nanoparticles are mixed with fuel, they should remain chemically stable for better and smoother fuel combustion operation. Optimization via machine learning15 and Response Surface Methodology (RSM) can be significantly applied for the design of biodiesel engines.16 These approaches provide advanced means for enhancing the efficiency, implementation, and environmental impact of biodiesel engines. A vital application is engine performance prediction and optimization. With different input parameters, ML models can be trained to forecast multiple factors like fuel efficiency, emissions, and overall engine health.17 Concurrently, RSM provides a disciplined approach for test design, modelling, and optimization, enabling researchers to identify optimal input variable combinations for enhanced performances.
In addition, these methods are crucial elements of emission-cutting initiatives. ML models could evaluate intricate correlations among biodiesel blends, engine operating conditions, and emissions. The findings may be employed to build successful emission-reduction measures.18 Simultaneously, RSM optimization aids in determining the best biodiesel blend to reduce emissions, while preserving or boosting the engine performance. Due to the synergy between ML and RSM, a holistic strategy for tackling both efficiency and environmental concerns is provided.19
LHR was applied in an engine using a ceramic coating with oxide on parts such as the crankshaft, chambers, and fittings at a thickness of 300 µm, which did not affect the physical size of the engine parts. Petroleum diesel was combined with 20% mahua biofuel and 5% ethanol. For comparison, the combustion capacity was investigated utilizing regular gasoline and contrasted with the biofuels using a combination of LHR and LTC methodologies. Lastly, the combination of LHR and LTC improved the combustion efficiency by up to 3.48%.20 The mixtures are run in a naturally inhaled, steady-state combustion ignition (CI) cylinder. Yttria stabilized zirconium (YSZ) was applied to the engine crowns of the instrumented cylinder to transform it into a heat rejecting (LHR) engine. Operating the motor on antioxidant-doped JME in LHR mode increased the thermal rate of release and highest cylinder pressures by approximately 4% and 7%, respectively, at the greatest load. The percentages of CO and unaltered HC discharges declined to an acceptable level of 10% and 13%, respectively, at the highest load performance; additionally, NO pollutants were reduced by 13% at the highest load level. The mileage and energy efficiency of the LHR engine increased by approximately 7% and 11%, respectively, when fully loaded.21 This investigation used two pistons around both the untreated and the additional polished one. The additional engine was coated with 300 µm-thick ZrO2 and 6–8 wt% Y2O3 ceramic substance, which is known as YSZ. A combination of Jatropha, also methyl alcohol (JME), and oil in proportions of 20% and 80% was created (JME20) and utilized as pilot fuel, while oxy-hydrogen (HHO) gases served as induction fuel for dual-fuel operations. HHO gas is free of greenhouse gases and a hydrogen-based sustainable fuel. The findings demonstrated that the effectiveness exhibited by the YSZ-coated pistons during the two dual-fuel activities (D100 + HHO and JME20 + HHO) was approximately 5.5% and 5.9% greater than that of D100 operating at the highest load, respectively. The equivalent dual-fuel processes resulted in a decreased level of HC, CO, and soot, regardless of the engine capacity.22 Experiments were conducted at peak load at an identical FIP (600 bar) with various FIT (19, 21, 23, 25, and 27 °BTDC) and fuel mixtures (D100, JOBD20, P10JD90, P20JD80, and P30JD70). In the beginning, the tests were conducted using solely diesel at the conventional injection rate and time. Furthermore, tests were performed by exchanging just diesel with extremely high responsiveness fuel (JOBD) at various infusion schedules, while less reactive fuels were delivered via the inlet pipe at equilibrium of 2 bar in various quantities. All quaternary fuel procedures with injections inclinations greater than 24°BTDC resulted in an increase in the piston pressure (89.82 bar), indicating better combustion with JOBD as HRF. Lower BTE levels (4.6%) were created because the electric production by the engine was reduced at 27°bTDC injecting, causing its pressure to be fairly elevated.23
| Ref. | Techniques | Parameters | Biodiesel | Remarks |
|---|---|---|---|---|
| 24 | Artificial neural network | Performance and emission parameters | Waste cooking oil | The ANN model demonstrated exceptional predictive accuracy across all engine output parameters, with correlation coefficients (r) exceeding 0.99 and R2 values surpassing 0.98 for every variable |
| 25 | ANN-ANFIS, RSM | Methanol molar ratio, catalyst amount, reaction time | Neem and castor | The ANFIS model outperformed the ANN in predicting yield, exhibiting higher R2 values, and thus superior forecasting accuracy |
| 26 | ANN, RSM | Split injection parameter | Ammonia-biodiesel | The ANN model achieved R2 values greater than 0.99 for all responses, demonstrating exceptional real-time predictive accuracy and outperforming RSM in reproducibility |
| 27 | ANFIS-NSGA-II and RSM | Engine load, biodiesel blend, and nanoparticle concentration | Leachate blends with nano-additives | The ANFIS-NSGA-II model produced responses with higher accuracy and efficiency than those generated by other models |
| 28 | ANFIS and RSM | EGT and all types of emissions | Nano diesel blended fuels | The test results closely align with the ANFIS predictions, demonstrating a high level of predictive accuracy |
| 29 | DTR, ABR, ETR, GBR, LGBM, and XGBR | Engine load, compression ratio, blend ratio | Aloe vera biodiesel with MWCNT nanoparticles | The XGBR model achieves the highest prediction accuracy compared to all other models |
| 30 | Decision tree and RSM | CR, injection time, injection pressure | Biogas-biodiesel blends | The decision tree-based models exhibited strong robustness, characterized by low mean squared errors |
| 31 | RSM | Load and compression ratios | Cassia fistula and Ricinus communis | RSM achieved correlation coefficients (R2) between 0.92 and 0.99 for all output parameters, demonstrating high predictive accuracy |
| 32 | RSM, gradient boosting (GBoost), extreme learning machine (ELM) | BP, LCV, blends | Moringa oleifera biodiesel with 1-hexanol and Zr2O3 nanoparticles | The ELM model achieved the highest accuracy (R2 = 0.9604), surpassing all other models |
| 33 | AMT ML and multi-objective optimization RSM | Varying engine torque, speed | Sunflower oil | The AWOA exhibits superior precision and a faster convergence rate compared to PSO |
| 34 | RSM with desirability | Engine load, biodiesel blend, and nanoparticle concentration | Mahua with CuO nanoparticles | RSM identified M20 with 60 ppm nanoparticle concentration at 80% load as the optimal condition (desirability score: 0.9), with the model attaining a mean absolute percentage error (MAPE) of just 3% |
Table 1 presents a comprehensive overview of the studies that have employed advanced machine learning (ML) and Response Surface Methodology (RSM) techniques to optimize the engine performance. These investigations highlight the synergistic advantages of combining the high predictive accuracy of ML with the robust optimization abilities of RSM to improve the engine efficiency and reduce emissions.
This study advances internal combustion (IC) engine technology through the study of a new blend of emulsified fuels, nano-Al2O3 additive, and compression ratio changes in a fly ash-coated LHR engine. It highlights the need for emission reduction via optimized combustion processes, a critical step towards compliance with strict environmental legislation and ensuring sustainable engine designs. The investigation of the synergy between emulsified fuels and nano-Al2O3 additives improves the current knowledge of innovative fuel technologies and provides a basis for more efficient, environmentally friendly fuel compositions. However, although the Response Surface Methodology (RSM) provides systematic and organized optimization, it seldom succeeds in identifying complex nonlinear relationships. Most existing research depended either on RSM or machine learning (ML) separately, thereby losing the chance to leverage their complementary benefits. Thus, this work fills this gap by integrating RSM with sophisticated ML models, like XGBoost, to improve the prediction accuracy and optimize the engine performance concurrently. The ensuing hybrid method presents a strong, scalable solution for optimizing biodiesel engines in accordance with worldwide sustainability objectives.
The combined application of RSM and XGBoost not only reflects methodological creativity but also yields practical knowledge regarding engine design and operational refinement. These results are a useful reference for engineers, researchers, and practitioners in the industry who want to enhance the performance and efficiency of IC engines. The capacity to successfully explore the high-dimensional parameter space of emulsified fuel-supplemented LHR engines reflects the power of advanced optimization methods in practical applications.
Improving the performance of IC engines, which is integral in a range of industries, is still key to realizing energy efficiency and environmental sustainability. The use of nano-Al2O3 additives and emulsified fuel in a fly ash-coated LHR engine represents a novel yet demanding research problem. Mechanistic appreciation of the intricate interactions between emulsified fuel formulations, nano-Al2O3 loading, and compression ratio variations is important for maximizing the combustion efficiency and reducing emissions. Therefore, this research is aimed at determining the best configurations and parameters that will ensure maximum efficiency in LHR engines through the employment of nano-enhanced emulsified fuels, and hence the development of the following research objectives.
(a) To investigate the impacts of varying CR on the combustion efficiency, power generation, and emissions in an LHR engine with a fly ash coating using emulsified fuel with a nano-Al2O3 additive.
(b) To study the impact of different nano-Al2O3 concentrations in emulsified fuel on the combustion behaviour, ignition characteristics, and engine performance as a whole.
(c) To utilize RSM to systematically optimize the compression ratio to achieve the maximum BTE considering the intricate interactions amongst the compression ratio, emulsified fuel composition, and nano-Al2O3 concentration.
(d) Using XGBoost modeling to forecast engine parameters and performance results as a function of compression ratio, emulsified fuel characteristics, and nano-Al2O3 concentration provides an integrated system understanding.
The choice of materials and techniques is an important factor for ensuring consistent results in any experimental study. For this research, the employment of cotton seed oil as a biodiesel feedstock was selected as a deliberate choice because of its prevalent availability as an agricultural waste and its inedibility, making it a suitable material for the production of sustainable fuel. Cotton seed biodiesel has a high cetane number, high oxygen content, and a safe flash point, which together lead to more efficient combustion and less harmful emissions. Additionally, its native lubricating attributes enhance engine longevity through the reduction of wear, thus longer engine life.
From a larger viewpoint, the use of cotton seed oil not only supports waste valorization and rural economic development but also fuels sustainable energy culture by minimizing reliance on fossil fuels. The compatibility of the biodiesel with nano-additives like aluminium oxide (Al2O3) adds to its usefulness, as the nanoscale particles facilitate purification of combustion quality, reduced emissions, and optimized engine performance. Therefore, the blend of cotton seed biodiesel and nano-additives is an attractive, environmentally friendly option for improving the efficiency and sustainability of compression ignition engines. Fig. 1 illustrates Micrograph of sample of fly ash Scanning Electron Microscope (SEM).
The application of thermal barrier coatings, such as fly ash, to LHR engines helps to improve their thermal efficiency by minimizing the heat loss. LHR engines have higher in-cylinder temperatures, which promote efficient combustion, because they retain more heat in their combustion chamber.36 This is especially beneficial for biodiesel blends, which have lower calorific values and higher viscosities. LHR engines also reduce the ignition delay, specific fuel consumption, and hydrocarbon and carbon monoxide emissions. Moreover, the application of fly ash coatings improves the engine durability under thermal stress, making LHR engines suitable for nano-enhanced biodiesel applications for cleaner and more efficient operation.37
LHR engines are a progressive type of engine with numerous possibilities to explore with the help of fruitful experimentation work. Following this, the piston crown and cylinder liner were coated with a thickness of 200 µm fly ash as an insulating material, as illustrated in Fig. 2 and 3. To maintain a standard compression ratio (CR) before coating, this section will deal with an important step that follows a systematic strategy.
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| Fig. 4 Layout of the mechanical stirrer arrangement for the preparation of the nano-emulsified fuel.35 | ||
The mixture was mixed well by agitating at 500 rpm. Throughout the agitation process, a surfactant such as Span 80 and Tween 80 (2% by volume) was mixed dropwise into the biodiesel water emulsion. The HLB value for the surfactant was considered 6.34 for this preparation. The mixture of biodiesel, water, and surfactant was kept under stirring for 40 min. According to earlier studies, if the water content in diesel fuel is greater than 10%, it prolongs the ignition delay. This results in uneven engine operation, and thus 10% water was used with biodiesel for emulsion. The detailed properties of the diesel and biodiesel along with the blends and nanoparticles are presented in Table 2. By adjusting the amounts of nanomaterial addition like mass fraction of Al2O3 in B20W10, several testing fuel samples were created. Here, the Al2O3 nanoparticle concentration reached 200 ppm.
| Property | Diesel | CSME | B20 | B50 | B20 + 100 ppm | ASTM |
|---|---|---|---|---|---|---|
| Viscosity (Cs) | 3.35 | 4.68 | 4.042 | 4.56 | 4.726 | ASTM D445 |
| Calorific value (kJ kg−1) | 42 858 |
39 528 |
39 496 |
39 484 |
42 058 |
ASTM 240 |
| Density (kg m−3) | 840 | 868 | 828 | 850 | 843 | ASTM D1298 |
| Flash point (°C) | 84 | 180 | 174 | 177 | 175 | ASTM 93 |
| Fire point (°C) | 94 | 123 | 96 | 86 | 84 | ASTM 93 |
The B20W10Al200 test fuel sample was created using an R-4C ultrasonicator. The ultrasonicator was run at 50 to 60 kHz frequency for 40 min to achieve the ideal emulsification. The color of the equipped nano-emulsified fuel sample is milky white due to the chemical reaction between the fuel and surfactant employed in this preparation process. However, this color did not negatively impact the performance aspects during testing in the engine operation.
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| Fig. 5 Experimental setup (a) and line diagram (b) of the diesel engine testing arrangement.20 (1) Engine base, (2) analyzer for exhaust gas, (3) house of the exhaust gas analyzer, (4) single-cylinder arrangement engine, (5) load cell, (6) dynamometer, (7) tachometer, (8) control system, (9) fuel burette and (10) fuel tank. | ||
| Factor | Specifications |
|---|---|
| Testing Engine specifications | |
| Type of engine | Direct injection (DI) diesel engine |
| Category | Single cylinder, four stroke |
| Power | 3.5 kW (@1500 ± 50 rpm) |
| Type of cooling | Water cooled |
| CR range | 12 : 1–18 : 1 |
| Injection variation | 0–25°BTDC |
| Combustion compartment | Semicircular bowl in piston type |
| Dynamometer | Water cooled with loading unit |
| Airbox | MS fabricated with orifice meter and manometer (100-0-100) |
| Fuel reservoir | Volume15 lit with measuring tube (0–450 mL) |
| Calorimeter | Pipe-in-pipe type |
| Data attainment software | ‘Soft-engine’ engine performance analysis software |
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|
| Transmitters, sensors, and indicators | |
| Fuel flow reader | DP transmitter, range 0–500 mm WC |
| Airflow transmitter | Pressure transmitter (−) 250 mm WC |
| Pressure sensors | Piezo type, range 5000 psi, with low noise cable |
| Temperature sensors and transmitters | PT100 (RTD) type, range 0–100 °C, output 4–20 mA (4 nos) |
| K (ungrounded) type, range 0–1200 °C, output 4–20 mA (2 nos) | |
| Load sensor and indicator | Strain measure-type load cell with digital pointer, range 0–50 kg |
| Speediness sensor and gauge | Resolution 1°, range (5500 rpm) with TDC pulse |
| Data acquisition device | NIUSB-6210, 16-bit, 250 kS s−1 |
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|
| Constants in the testing engine | |
| Pulse per revolution | 360° |
| No. of cycles | 10 |
| Fuel measuring interval | 60 s |
| Speed scanning intervals | 2000 ms |
| Bore × stroke | 87.6 mm × 110 mm |
| Capacity | 662 cc |
| Cavity diameter | 2 mm |
| Dynamometer arm length | 18 mm |
| Linking rod length | 235 mm |
A special program algorithm was adopted in the data processing unit, where it takes an average of more than 50 uninterrupted cycles to get an effective assessment of the heat release rate, time for the combustion process, etc. Under the initial conditions, the testing process started with neat diesel as the test fuel. This step worked as a warm-up step for the engine, and then it was substituted for the nanoparticle-emulsified cotton seed biodiesel fuel. To clean the fuel line and fuel injection system, the engine ran on neat diesel fuel at the end.
This surface enables investigators to understand the behavior of the system within the experimental area, and thus ascertain the optimal conditions that lead to the desired outcome. RSM facilitates the build-up of proper models, reflecting the intricacies of the system being studied using statistical methods such as regression analysis. RSM is applied in different fields, ranging from engineering and physics to biological sciences, to maximize processes as well as performances. It is possible for researchers to comprehend the performance of a system and successfully identify the most appropriate operating conditions by making systematic changes to the input variables while observing the resulting changes in the response variable. Additionally, RSM is an economical approach as it minimizes the number of experimental runs necessary for solid outcomes.41
The focus on breaking the challenges facing gradient boosting methods, such as over fitting and computational inefficiency, sets XGBoost apart. XGBoost finds a balance between model complexity and accuracy using regularization methods and a new objective function, which consists of both a loss function and a regularized function.43 This makes it less prone to over fitting, irrespective of big data. The ‘gradient boosting’ process of this algorithm involves the stepwise construction of decision trees to correct flaws in earlier models, constantly improving the overall predicting capacity. XGBoost further introduces complexity by employing a stronger optimization method, making it particularly well-suited to handle enormous databases containing disparate feature types. Its ability to identify complex data patterns and produce feature importance scores increase the interpretability, while making it applicable in real-world scenarios.44
Also, its speed, flexibility, and ability to handle various types of data are all reasons for its use in applications ranging from banking to healthcare. In addition, the integration of XGBoost with Python and other programming languages enables straightforward installation and easy integration with existing ML pipelines. Fundamentally, XGBoost is the algorithm of choice for practitioners seeking a reliable, fast algorithm that performs superbly in predicting accuracy and generalization across a broad variety of datasets.45
The overall process flow chart is provided in Fig. 6 for a better understanding.
By clearly explaining the concept and utilizing the appropriate terminology, the revised content enhances the understanding of the relationship among the compression ratio, NHR, and combustion process in the engine.
This finding suggests that irrespective of the specific CR value, the highest in-cylinder pressure is consistently achieved at a similar crank angle. In this case, the compression ratio of 18 yields the maximum peak pressure. The precise crank angle and corresponding in-cylinder pressure provide valuable insights into the combustion process and engine performance.48
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| Fig. 9 Impact of BP on BTE for different CR: (a) test values, (b) contour plot, (c) surface plot and (d) predicted vs. actual values. | ||
The data gathered through lab-based experiments was used to for analysis of variance (ANOVA) to find the link between different data columns. The outcomes of ANOVA are listed in Table 4. The model has an F-value of 150.33, indicating that it is statistically significant. A “model F-value” of this magnitude arising entirely from noise is only 0.01% likely. Model terms are considered relevant when the value of “Prob > F” is less than 0.0500. The significant model terms in this case are A, B, and A2. Values greater than 0.1000 indicate that the model terms are unimportant. Model reduction approaches can improve the model if it contains many insignificant terms. The developed model for BTE is given as eqn (1). The model was used to predict values at different engine settings. A comparison of the actual and model-predicted table values is shown in Fig. 9a. It can be observed that the model performed well given that most of the point lies on the best-fit line. The contour plot (Fig. 9b) and surface plot (Fig. 9c) depict that the peak BTE efficiency is achieved at a higher engine load and compression ratio.29 Fig. 9d represents the predicted vs. actual values of BTE, where it can be observed in the graph that both values are very close and approximately linear (Fig. 9d).
| BTE = 18.395 + 9.15 × BP − 2.04 × CR + 0.198 × BP × CR − 1.96 × BP2 + 0.073 × CR2 | (1) |
| Source | Sum of squares | dF | Mean of squares | F-value | p-Value prob > F | |
|---|---|---|---|---|---|---|
| Model | 839.81 | 5 | 167.96 | 150.33 | <0.0001 | Significant |
| A-BP | 764.06 | 1 | 764.06 | 683.86 | <0.0001 | |
| B-CR | 9.01 | 1 | 9.01 | 8.06 | 0.0124 | |
| AB | 0.52 | 1 | 0.52 | 0.46 | 0.5060 | |
| A2 | 55.40 | 1 | 55.40 | 49.58 | <0.0001 | |
| B2 | 0.025 | 1 | 0.025 | 0.022 | 0.8836 | |
| Residual | 16.76 | 15 | 1.12 | |||
| Cor total | 856.57 | 20 |
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| Fig. 10 Impact of BP on BSFC for different CR: (a) test values, (b) contour plot, (c) surface plot and (d) predicted vs. actual values. | ||
The model F-value, a substantial 208.48, emphasizes the robustness of the model, showing an insignificant 0.01% chance of having such a huge value arising due to unpredictability. The results of ANOVA are listed in Table 5. Regarding the model relevance, terms A, B, and A2 stand out (Prob > F of 0.0500), while values over 0.1000 indicate insignificance. If there are many inconsequential model terms (except those required for hierarchy), a model reduction could improve its effectiveness. Std. Dev., R2 (0.9858), and Adeq. Precision (41.031) constitute key metrics that add to the reliability of the model, and the significant “Pred R-Squared” (0.9735) fits nicely with the “Adj R-Squared” (0.9811), emphasizing the predictive accuracy. The Adeq. Precision ratio, which is more than 4, emphasizes a favorable signal-to-noise ratio, enabling effective design space exploration and enhancing the practical usability of the model. The mathematical model developed using ANOVA is given in eqn (2). The model was used to forecast values at various engine settings. It can be seen that the model performed well because the majority of the points are on the best-fit line. The lowest BSFC was at a higher engine load and compression ratio, as shown by the contour plot (Fig. 10b) and the surface plot (Fig. 10c). Fig. 10d represents the predicted vs. actual values of BSFC and it can be observed that both values are very close and approximately linear, as shown in the graph. Hence, the model is more suitable for future studies.
| BSFC = 1.0211 − 0.474 × BP + 0.0128 × CR + 0.0022 × BP × CR + 0.074 × BP2 − 0.00107 × CR2 | (2) |
| Source | Sum of squares | dF | Mean of squares | F-value | p-Value prob > F | |
|---|---|---|---|---|---|---|
| Model | 0.64 | 5 | 0.13 | 208.48 | <0.0001 | Significant |
| A-BP | 0.52 | 1 | 0.52 | 842.73 | <0.0001 | |
| B-CR | 5.315E-003 | 1 | 5.315E-003 | 8.59 | 0.0103 | |
| AB | 6.191E-005 | 1 | 6.191E-005 | 0.10 | 0.7561 | |
| A2 | 0.11 | 1 | 0.11 | 170.51 | <0.0001 | |
| B2 | 5.357E-006 | 1 | 5.357E-006 | 8.661E-003 | 0.9271 |
Fig. 11 illustrates the impact of brake power (BP) on HC emissions. Among the tested fuels, diesel had the lowest HC emissions of 51 ppm due to its good combustion property. The emulsified cotton seed biodiesel blends showed slightly higher HC emissions of 64 ppm at CR16, 59 ppm at CR17 and 55 ppm at CR18. Especially, CR16 demonstrated 25.5% more HC emissions than diesel, explaining the reason for the poor atomization and lower in-cylinder temperatures at CR16, which prolonged the ignition delay and led to unburned fuel. As the CR increased, the thermodynamic conditions became more favorable with regard to fuel atomization and enhancement of flame front propagation. The nanoparticles of aluminum oxide enhanced micro-explosions and burned more uncombusted hydrocarbons. This was most effective at a CR of 18. The results show that exhaust HC emissions can be reduced by optimizing the CR and using nano-emulsified biodiesel to promote more complete combustion. These observations highlight the importance of optimizing the CR to achieve a higher burning rate and minimize HC emissions. Hydrocarbon outputs from the biodiesel blend arise from the aerobic biofuel section, facilitating a more thorough burning of chemical forms. The breathable air promotes enhanced oxidative damage of HCs, specifically at the higher levels accomplished in the LHR engine arrangement.
In contrast to the other tested samples, the results showed that diesel fuel had the highest NOx emissions. Notably, the NOx emissions at CR16 were 13.5% lower than diesel emissions. This can be explained by the lower ignition temperature brought on by the lower CR of 16. NOx emissions diminish under every load scenario as the perfect level increases. When the combustion chamber engines are coated with the LHR material, oxides of nitrogen are diminished due to the smaller amount of oxygen and decreased flame temperature.
These findings highlight the importance of selecting an appropriate compression ratio to minimize the smoke opacity in dual-fuel mode by considering the influence of BP and optimizing the CR.45
| Run | BP, kW | CR | BTE, % | BsFC, kg kW−1 h−1 | NOx, ppm | HC, ppm | CO, % | Smoke OP. % |
|---|---|---|---|---|---|---|---|---|
| 1 | 0.32 | 16.00 | 7.82 | 0.834 | 95 | 146 | 0.168 | 4.9 |
| 2 | 0.86 | 16.00 | 14.89 | 0.595 | 198 | 121 | 0.141 | 8.5 |
| 3 | 1.35 | 16.00 | 16.58 | 0.512 | 245 | 105 | 0.138 | 9.3 |
| 4 | 1.71 | 16.00 | 21.85 | 0.39 | 429 | 99 | 0.135 | 11.6 |
| 5 | 2.20 | 16.00 | 22.25 | 0.36 | 508 | 88 | 0.127 | 12.3 |
| 6 | 2.56 | 16.00 | 24.74 | 0.33 | 610 | 82 | 0.121 | 15.8 |
| 7 | 3.42 | 16.00 | 27.15 | 0.295 | 842 | 64 | 0.114 | 22.3 |
| 8 | 0.32 | 17.00 | 8.12 | 0.814 | 101 | 128 | 0.164 | 3.6 |
| 9 | 0.86 | 17.00 | 15.48 | 0.579 | 220 | 114 | 0.138 | 7.1 |
| 10 | 1.35 | 17.00 | 17.25 | 0.501 | 265 | 101 | 0.133 | 8.2 |
| 11 | 1.71 | 17.00 | 22.63 | 0.36 | 465 | 91 | 0.13 | 8.8 |
| 12 | 2.20 | 17.00 | 23.25 | 0.33 | 535 | 83 | 0.124 | 11.4 |
| 13 | 2.56 | 17.00 | 25.54 | 0.312 | 625 | 75 | 0.116 | 12.8 |
| 14 | 3.42 | 17.00 | 28.01 | 0.289 | 858 | 59 | 0.108 | 19.8 |
| 15 | 0.32 | 18.00 | 8.35 | 0.785 | 105 | 115 | 0.16 | 3.3 |
| 16 | 0.86 | 18.00 | 15.98 | 0.567 | 224 | 105 | 0.128 | 6.5 |
| 17 | 1.35 | 18.00 | 18.98 | 0.465 | 321 | 82 | 0.125 | 7.5 |
| 18 | 1.71 | 18.00 | 23.12 | 0.345 | 498 | 85 | 0.118 | 8.1 |
| 19 | 2.20 | 18.00 | 23.99 | 0.315 | 565 | 74 | 0.12 | 10.4 |
| 20 | 2.56 | 18.00 | 26.85 | 0.293 | 644 | 69 | 0.096 | 12.2 |
| 21 | 3.42 | 18.00 | 29.03 | 0.269 | 866 | 55 | 0.104 | 19.3 |
| Control factors | Response variables | |||||||
|---|---|---|---|---|---|---|---|---|
| BP | CR | BTE | BSFC | NOx | HC | CO | Smoke Op | Desirability |
| 2.49 | 18 | 26.43 | 0.2778 | 636 | 68.23 | 0.106 | 12.43 | 0.751 |
The methodology starts with the data acquisition and preprocessing of a dataset comprising different CR and braking power values. These are crucial inputs as they represent the inherent characteristics of the engine under different operating conditions. The response variables like BTE, BSFC, NOx emissions, CO, HC emissions, and smoke levels are closely monitored and measured to capture the diverse engine performances and emissions characteristics. The data was randomly divided in a 70
:
30 ratio for training and testing. The grid search-based hyperparameter optimization was employed in this study. The hyperparameter range and optimized values are listed in Table 9.
XG Boost, which has proven ability to cope with high-order interactions and various data sources, is then used to develop prediction models. The approach builds an ensemble of decision trees iteratively and learns from the patterns of the training data for predicting the response variables accurately. Regularization methods in XGBoost reduce the risk of overfitting, ensuring strong generalization to new, unseen data. Validation and optimization of XGBoost models are necessary steps within the research method. The data is split into training and test sets, allowing the model performance to be measured against independent information. Increasing the predictive power of the model, hyper parameter tuning and cross-validation strategies enhance its reliability and accuracy in modeling the complex interactions among CR, braking power, and engine reaction variables.
The correlations between data columns are shown in Fig. 16 as a correlation heat map. After the model was created, it was used for prediction. The statistical measures in Table 8 provide a detailed evaluation of how well a predictive model performs during the training and testing phases, highlighting important engine response features. R2, mean squared error (MSE), and mean absolute percentage error (MAPE) are some of the measures used to gain more detailed insight into the accuracy of the model and its prediction ability.
| Train R2 | Train MSE | Train MAPE | Test R2 | Test MSE | Test MAPE | |
|---|---|---|---|---|---|---|
| BTE | 1 | 0.0004 | 0.082 | 0.9288 | 0.7299 | 3.4051 |
| BSFC | 0.9999 | 0.0000009 | 0.21458 | 0.9931 | 0.0003 | 2.1951 |
| NOx | 0.9999 | 0.3919 | 0.2259 | 0.9848 | 500.34 | 9.365 |
| HC | 0.9989 | 0.352331 | 0.5066 | 0.9026 | 103.46 | 9.317 |
| CO | 0.9517 | 0.00001 | 2.0451 | 0.9137 | 0.00002 | 3.745 |
| Smoke Op | 0.996 | 0.06999 | 2.314 | 0.942 | 2.38 | 7.674 |
| Hyperparameter | Search range | BTE | BSFC | NOx | HC | CO | Smoke OP. |
|---|---|---|---|---|---|---|---|
| Learning_rate | [0.01, 0.05, 0.1] | 0.1 | 0.5 | 0.1 | 0.1 | 0.5 | 0.05 |
| Max_depth | [3, 4, 5] | 3 | 5 | 5 | 3 | 4 | 3 |
| n_estimators | [50, 100, 150] | 150 | 150 | 150 | 100 | 50 | 150 |
| Subsample | [0.7, 0.9, 1.0] | 0.9 | 0.7 | 0.7 | 0.7 | 1 | 0.7 |
Table 8 and Fig. 17 depict the performance of the XGB models applied to predict BTE, BSFC, NOx, HC, CO, and SO using key input features. The model does a great job at training for BTE (Fig. 17a), with R2 = 1 and MSE = 0.0004, which means it fits perfectly. The excellent generalization and ability of the model to capture the changes in thermal efficiency across a range of CR and BP circumstances are confirmed by the test R2 of 0.9288, MSE of 0.7299, and MAPE of 3.41%. The model has R2 values of 0.9999 (train) and 0.9931 (test), which are almost excellent for BSFC (Fig. 17b). The MSE values are quite low, and the test MAPE of 2.20% shows that the predictions are very accurate. This shows that XGB does a good job of modelling BSFC, which is load sensitive, particularly when the fuel-air conditions are different. The R2 values for the train and test sets for NOx are 0.9999 and 0.9848, respectively, as shown in Fig. 17c and Table 8. The test MSE is also quite high at 500.34, which suggests that the results may not always be accurate given that NOx generation is nonlinear. However, a test MAPE of 9.37% is acceptable given the complicated thermal NOx dynamics. The train R2 = 0.9989 and test R2 = 0.9026 in the HC model show that the model learned well (Fig. 17d). However, the test MAPE of 9.32% shows that there was slightly more error, perhaps because of combustion instability at lower BP and emissions during cold starts. The train and test R2 scores for the CO model are 0.9517 and 0.9137, respectively (Fig. 17e). The MSE values are quite low, while the test MAPE is 3.75%. Although CO depends on the intensity of the mixture and the amount of oxygen available, these findings imply that the CO predictions are consistent. Lastly, the SO model gives R2 values of 0.996 for the training set and 0.942 for the test set, as well as a test MSE of 2.38 and a test MAPE of 7.67% (Fig. 17f). These numbers show that XGB does a good job of capturing how soot moves when there is a load and when the CR changes. Overall, all the models train well and make good predictions, with test R2 values more than 0.90 in all situations. This shows that XGB and the modified hyperparameters are good at modelling complicated engine behaviour with high accuracy.
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| Fig. 17 Model prediction vs. actual data. (a) BTE, (b) BSFC, (c) NOx, (d) HC, (e) CO and (f) smoke opacity. | ||
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| Fig. 18 SHAP values for feature analysis for (a) BTE, (b) BSFC, (c) NOx, (d) HC, (e) CO and (f) smoke opacity. | ||
Fig. 18d (HC) shows that decreasing the BP greatly lowers HC emissions, whereas CR has a more random effect. The trend shows that there is incomplete combustion at lower loads, which increases the amount of unburned hydrocarbons. Fig. 18e (CO) indicates that both characteristics have a SHAP effect that is close to zero. This means that the model thinks these features are not very good at predicting CO. This might be because CO is sensitive to other parameters that affect combustion, including the temperature and the air-fuel ratio, which are not included in this narrow collection of features. Lastly, Fig. 18f (smoke opacity) shows that greater BP levels make the smoke levels increases, whereas higher CR levels make them decrease slightly. This is consistent with what happens in real life, where a higher load produces soot, while a high CR makes combustion more complete. These SHAP charts make the XGBoost models easier to understand, confirm the engine performance patterns, and build confidence in the models.
Furthermore, this research propels fuel technology by proving the suitability of emulsified fuels with nano-Al2O3 additive to enhance combustion characteristics to a high degree. This development could pave the way to devising fuel blends that are both environmentally friendly and cost-effective. These findings can totally revolutionize the operation of machines and vehicles by allowing industries and governments to make informed choices that will determine the future of energy systems and transportation. The improvements in methodology brought by the research in applying advanced optimization methods, such as RSM and XGBoost modeling, have broader implications for experimental design and data analysis. The capability of these techniques to effectively search the complex parameter space of fuel-supplied engines with emulsified fuels sets a benchmark for subsequent research studies seeking to optimize complex systems.
The approaches used in this work may be crucial in tackling issues in various scientific and technical fields as the need for sustainable energy solutions grows. The results of this study can essentially be applied to realize methodological breakthroughs, technological innovation, and environmental stewardship. According to this research, emulsified fuels and nano-Al2O3 additives are potential components in the continuing effort to help society move to cleaner and more efficient energy sources in the quest for sustainable internal combustion engine technology.
Overall, the incorporation of nano-biodiesel blends in thermal barrier coatings and intelligent modeling presents a promising route toward increasing the efficiency and minimizing environmental effects in compression ignition engines, moving toward sustainable engine technology.
• A more complete picture of the possible trade-offs and synergies in engine performance may be obtained by integrating other factors such as various coating materials, emulsification processes, and types of nanoparticle.
• Broadening the scope of this study to encompass diverse engine categories and operational circumstances, engines using nano-Al2O3 additives and emulsified fuels may also be conducted to solve engine wear and maintenance issues.
• Advanced computer models and simulations might be used to supplement the experimental results, enabling a more thorough examination of optimization techniques and combustion processes.
| Al2O3 | Aluminum oxide |
| BTE | Brake thermal efficiency |
| BSFC | Brake specific fuel consumption |
| BP | Brake power |
| CO | Carbon monoxide |
| CO2 | Carbon dioxide |
| CR | Crank angle |
| HC | Hydrocarbon |
| CR16 | Compression ratio of 16 |
| LHR | Low heat rejection |
| RSM | Response surface methodology |
| SEM | Scanning electron microscopy |
| MAPE | Mean absolute percentage error |
| MSE | Mean squared error |
| ML | Machine learning |
| NOx | Nitrogen emissions |
| HRR | Heat release rate |
| NHR | Net heat release rate |
| Ppm | Parts per minute |
| XG | Extreme gradient boosting |
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