Deqing Mei
Current Organizations / Institutes
The organizations/institutes from the scholar's latest article
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Deqing Mei has a total of 105 co-authors. Here are the top co-authors by number of shared publications:
Yinnan Yuan
College of Energy Soochow University Suzhou China
11 shared publications- Lei Zuo
School of Energy and Power Engineering, Jiangsu University, Zhenjiang 212013, China
8 shared publications Dongbao Wang
School of Energy and Power Engineering, Jiangsu University, Zhenjiang 212013, China
7 shared publications- Haojie Xu
Jiangsu University, China
7 shared publications Jiang Yao
School of Energy and Power Engineering, Jiangsu University, Zhenjiang 212013, China
7 shared publicationsTianyue Zhao
School of Energy and Power Engineering, Jiangsu University, Zhenjiang 212013, China
7 shared publications
Latest Publications
- 1 February 2027
- Published by American Society of Civil Engineers (ASCE) in Journal of Energy Engineering
- Vol. 153 (1)
Mechanism Construction and Combustion Characteristics Analysis of Diesel Fuel Blended with Nano-CeO 2
The catalytic influence of CeO 2 nanoparticles on diesel combustion was investigated through detailed kinetic modeling. A diesel surrogate consisting of n - dodecane ( NC 12 H 26 ) and p-xylene ( C 8 H 10 ) was adopted to represent the major chemical characteristics of real diesel fuel. A catalytic reaction mechanism describing the redox behavior of cerium dioxide ( CeO 2 ) was incorporated into the base fuel mechanism to construct a simplified kinetic framework for CeO 2 nanofuels. Combustion simulations were performed under various initial temperatures and pressures to evaluate the influence of CeO 2 nanoparticles on ignition behavior and combustion reactivity. The results indicate that the addition of CeO 2 significantly promotes the formation of OH and H 2 O 2 radicals at relatively low temperatures, leading to shorter ignition delay and enhanced heat release rates. At higher temperatures, combustion is dominated by rapid thermal decomposition of fuel molecules, which reduces the dependence of the system on catalytic radical generation and weakens the catalytic influence of CeO 2 . Furthermore, CeO 2 nanoparticles accelerate hydrocarbon oxidation and CO conversion while also enhancing nitrogen oxides ( NO x ) reduction reactions. Reaction pathway analysis shows that the primary oxidation pathways of the base fuel remain unchanged, whereas the catalytic reactions mainly affect radical formation and intermediate oxidation processes. These findings provide insight into the catalytic combustion mechanism of CeO 2 nanofuels and their potential for improving diesel combustion performance.
- 1 February 2027
- Published by American Society of Civil Engineers (ASCE) in Journal of Energy Engineering
- Vol. 153 (1)
Mechanism Construction and Combustion Characteristics Analysis of Diesel Fuel Blended with Nano-CeO 2
The catalytic influence of CeO 2 nanoparticles on diesel combustion was investigated through detailed kinetic modeling. A diesel surrogate consisting of n - dodecane ( NC 12 H 26 ) and p-xylene ( C 8 H 10 ) was adopted to represent the major chemical characteristics of real diesel fuel. A catalytic reaction mechanism describing the redox behavior of cerium dioxide ( CeO 2 ) was incorporated into the base fuel mechanism to construct a simplified kinetic framework for CeO 2 nanofuels. Combustion simulations were performed under various initial temperatures and pressures to evaluate the influence of CeO 2 nanoparticles on ignition behavior and combustion reactivity. The results indicate that the addition of CeO 2 significantly promotes the formation of OH and H 2 O 2 radicals at relatively low temperatures, leading to shorter ignition delay and enhanced heat release rates. At higher temperatures, combustion is dominated by rapid thermal decomposition of fuel molecules, which reduces the dependence of the system on catalytic radical generation and weakens the catalytic influence of CeO 2 . Furthermore, CeO 2 nanoparticles accelerate hydrocarbon oxidation and CO conversion while also enhancing nitrogen oxides ( NO x ) reduction reactions. Reaction pathway analysis shows that the primary oxidation pathways of the base fuel remain unchanged, whereas the catalytic reactions mainly affect radical formation and intermediate oxidation processes. These findings provide insight into the catalytic combustion mechanism of CeO 2 nanofuels and their potential for improving diesel combustion performance.
- 1 March 2026
- Published by AIP Publishing in Journal of Renewable and Sustainable Energy
- Vol. 18 (2)
Combustion and emission performance of biodiesel–ethanol renewable fuels: Experimental study and machine learning prediction
Considering the complementary fuel properties between biodiesel and ethanol, biodiesel–ethanol renewable fuels with different blending ratios were formulated. Under various operating conditions, the effects of different blending ratios of renewable fuels on combustion and emission performances were experimentally investigated. Results showed that equivalent specific fuel consumption (ESFC) was highly sensitive to operating conditions: fuel economy was inferior to diesel under low and medium loads but superior under high loads. Under 50% load, ethanol's cooling effect reduced in-cylinder temperature and delayed combustion, lowering indicated mean effective pressure (IMEP); under 100% load, ethanol's higher volatility improved fuel-air mixing, accelerating combustion and increasing IMEP. Emissions were governed by load-dependent thermal conditions and fuels' oxygenated nature: low and medium loads saw ethanol's high latent heat create a low-temperature environment, suppressing nitrogen oxides (NOx) but increasing hydrocarbon (HC) and carbon monoxide (CO); high loads enhanced combustion via oxygen, slightly raising NOx but significantly reducing HC and CO. Machine learning evaluation indicated that the artificial neural network (ANN) and support vector machine (SVM) performed best for ESFC prediction; SVM and multiple linear regression were most effective for IMEP; and ANN yielded the best results for NOx prediction. This study provides a theoretical basis and practical support for the intelligent prediction and optimization of renewable fuel combustion performance.
- 1 March 2026
- Published by AIP Publishing in Journal of Renewable and Sustainable Energy
- Vol. 18 (2)
Combustion and emission performance of biodiesel–ethanol renewable fuels: Experimental study and machine learning prediction
Considering the complementary fuel properties between biodiesel and ethanol, biodiesel–ethanol renewable fuels with different blending ratios were formulated. Under various operating conditions, the effects of different blending ratios of renewable fuels on combustion and emission performances were experimentally investigated. Results showed that equivalent specific fuel consumption (ESFC) was highly sensitive to operating conditions: fuel economy was inferior to diesel under low and medium loads but superior under high loads. Under 50% load, ethanol's cooling effect reduced in-cylinder temperature and delayed combustion, lowering indicated mean effective pressure (IMEP); under 100% load, ethanol's higher volatility improved fuel-air mixing, accelerating combustion and increasing IMEP. Emissions were governed by load-dependent thermal conditions and fuels' oxygenated nature: low and medium loads saw ethanol's high latent heat create a low-temperature environment, suppressing nitrogen oxides (NOx) but increasing hydrocarbon (HC) and carbon monoxide (CO); high loads enhanced combustion via oxygen, slightly raising NOx but significantly reducing HC and CO. Machine learning evaluation indicated that the artificial neural network (ANN) and support vector machine (SVM) performed best for ESFC prediction; SVM and multiple linear regression were most effective for IMEP; and ANN yielded the best results for NOx prediction. This study provides a theoretical basis and practical support for the intelligent prediction and optimization of renewable fuel combustion performance.
- 1 December 2025
- Published by American Society of Civil Engineers (ASCE) in Journal of Energy Engineering
- Vol. 151 (6)
Experimental Study on the Combustion Performance of Carbon-Based Nano-Fuel Droplets
- 1 December 2025
- Published by American Society of Civil Engineers (ASCE) in Journal of Energy Engineering
- Vol. 151 (6)
Experimental Study on the Combustion Performance of Carbon-Based Nano-Fuel Droplets
- 21 October 2025
- Published by Elsevier in International Journal of Hydrogen Energy
- Vol. 187
Kinetic modeling and optimization of ammonia/n-heptane combustion for HCCI engine applications
- 21 October 2025
- Published by Elsevier in International Journal of Hydrogen Energy
- Vol. 187
Kinetic modeling and optimization of ammonia/n-heptane combustion for HCCI engine applications
- Open Access
Study on Swirling Flow and Spray Characteristics of Central Stage Direct Injection Combustor
To investigate the physical phenomena interactions between airstream and liquid injection or droplets within a complex multi-stage swirl flow field, this study investigated the flow field and spray characteristics in a central stage direct injection combustor with a variety of optical diagnostic techniques, including using time-resolved particle image velocimetry (PIV) to measure the swirl flow field, using time-resolved planar Mie scattering (PMie) to measure the spray pattern, and using a laser particle size analyzer (LPSA) to measure the spray droplet size and its distribution. The results indicate that the lip recirculation zone (LRZ) and the swirl jet zone (SJZ) significantly influence droplet spatial and size distribution characteristics, such as spray penetration, cone angle, and droplet size. Due to the unique characteristics of the dual-stage swirl atomizer, the spray cone angle and penetration do not increase monotonically with the gas Weber number (). For the pilot stage, at a constant , both the spray cone angle and penetration increase with higher fuel injection velocity. At different fuel injection velocities, the spray penetration increases with rising . When the fuel injection velocity is low, the cone angle initially increases and then decreases as grows. The results about the effect of on droplet size distribution further support this conclusion. The Sauter mean diameter (SMD) of the main and pilot stage decreases with increasing relative pressure drop of air until reaching a stable state. The aerodynamic shear of the swirling airstream is sufficient to promote thorough fuel atomization, ensuring that the SMD remains low at the whole operating condition. Therefore, for the dual-stage swirl atomizer investigated in this study, good atomization can be achieved under low operating conditions, which provides a theoretical foundation and data support for the improvement and design of a low-emission, high-performance atomizer.Open AccessStudy on Swirling Flow and Spray Characteristics of Central Stage Direct Injection Combustor
To investigate the physical phenomena interactions between airstream and liquid injection or droplets within a complex multi-stage swirl flow field, this study investigated the flow field and spray characteristics in a central stage direct injection combustor with a variety of optical diagnostic techniques, including using time-resolved particle image velocimetry (PIV) to measure the swirl flow field, using time-resolved planar Mie scattering (PMie) to measure the spray pattern, and using a laser particle size analyzer (LPSA) to measure the spray droplet size and its distribution. The results indicate that the lip recirculation zone (LRZ) and the swirl jet zone (SJZ) significantly influence droplet spatial and size distribution characteristics, such as spray penetration, cone angle, and droplet size. Due to the unique characteristics of the dual-stage swirl atomizer, the spray cone angle and penetration do not increase monotonically with the gas Weber number (). For the pilot stage, at a constant , both the spray cone angle and penetration increase with higher fuel injection velocity. At different fuel injection velocities, the spray penetration increases with rising . When the fuel injection velocity is low, the cone angle initially increases and then decreases as grows. The results about the effect of on droplet size distribution further support this conclusion. The Sauter mean diameter (SMD) of the main and pilot stage decreases with increasing relative pressure drop of air until reaching a stable state. The aerodynamic shear of the swirling airstream is sufficient to promote thorough fuel atomization, ensuring that the SMD remains low at the whole operating condition. Therefore, for the dual-stage swirl atomizer investigated in this study, good atomization can be achieved under low operating conditions, which provides a theoretical foundation and data support for the improvement and design of a low-emission, high-performance atomizer. - 19 February 2023
- Published by Taylor & Francis in Combustion Science and Technology
- Vol. 196 (15) , 3576-3591
Droplet evaporation characteristics of hydrogenated biodiesel-ethanol-diesel ternary fuel
A multi-component blend of highly volatile ethanol with low volatile hydrogenated biodiesel and diesel is the subject of study. The internal vapor bubble dynamics and evaporation characteristics of individual droplets at high temperatures were investigated. The evaporation characteristics of droplet normalized square diameter and droplet lifetime of the blends of hydrogenated biodiesel, ethanol, and diesel were captured by means of the hanging droplet method and high-speed microscopic imaging in a constant temperature heating furnace. It is revealed that the rise in ambient temperature contributes to increasing the evaporation rate of fuel droplets and intensifies the micro explosion during evaporation and shortens the evaporation of droplets to a certain extent; Compared to diesel, the inhibition effect of evaporation is stronger with the increase of hydrogenated biodiesel in binary fuels and compared with binary fuels, ethanol in ternary fuels promotes micro explosions and shortens droplet evaporation; The droplet evaporation of binary fuels shows three typical phases of ethanol domination, ethanol, and diesel co-domination and co-evaporation of all three in sequence.
- 19 February 2023
- Published by Taylor & Francis in Combustion Science and Technology
- Vol. 196 (15) , 3576-3591
Droplet evaporation characteristics of hydrogenated biodiesel-ethanol-diesel ternary fuel
A multi-component blend of highly volatile ethanol with low volatile hydrogenated biodiesel and diesel is the subject of study. The internal vapor bubble dynamics and evaporation characteristics of individual droplets at high temperatures were investigated. The evaporation characteristics of droplet normalized square diameter and droplet lifetime of the blends of hydrogenated biodiesel, ethanol, and diesel were captured by means of the hanging droplet method and high-speed microscopic imaging in a constant temperature heating furnace. It is revealed that the rise in ambient temperature contributes to increasing the evaporation rate of fuel droplets and intensifies the micro explosion during evaporation and shortens the evaporation of droplets to a certain extent; Compared to diesel, the inhibition effect of evaporation is stronger with the increase of hydrogenated biodiesel in binary fuels and compared with binary fuels, ethanol in ternary fuels promotes micro explosions and shortens droplet evaporation; The droplet evaporation of binary fuels shows three typical phases of ethanol domination, ethanol, and diesel co-domination and co-evaporation of all three in sequence.
- Open Access
Numerical Investigation on Mechanism of Swirling Flow of the Prefilming Air-Blast Fuel Injector
Prefilming air-blast atomizers are widely used in modern gas turbine combustors. Due to insufficient awareness of the coupling mechanism of multi-stage swirling flow in gas turbines, there is a lack of effective methods for flow field optimization in combustor. In this study, the effect of some critical parameters on the flow field of a prefilming air-blast atomizer was analyzed with CFD. The parameters include the angle and number of the first swirler blades, the angle of the second swirler blades and the angle of sleeve. Furthermore, the coupling mechanism of two-stage swirling airflows of prefilming air-blast atomizer was discussed. Moreover, the influence of the interaction between two-stage counter swirling airflows on the characteristics of flow field was explained. The results show that with the increase in SNi, the axial length of the primary recirculation zone decreased, while the radial width increased. The starting position of primary recirculation zone (PRZ) moves forward with the increase in SNo. Reducing the sleeve angle β helps to form the primary recirculation zone. The results indicate that it is the transition of tangential velocity of airflow to radial velocity that promotes the formation of the PRZ. These results provide theoretical support for optimization of the flow field in swirl combustor.
Open AccessNumerical Investigation on Mechanism of Swirling Flow of the Prefilming Air-Blast Fuel Injector
Prefilming air-blast atomizers are widely used in modern gas turbine combustors. Due to insufficient awareness of the coupling mechanism of multi-stage swirling flow in gas turbines, there is a lack of effective methods for flow field optimization in combustor. In this study, the effect of some critical parameters on the flow field of a prefilming air-blast atomizer was analyzed with CFD. The parameters include the angle and number of the first swirler blades, the angle of the second swirler blades and the angle of sleeve. Furthermore, the coupling mechanism of two-stage swirling airflows of prefilming air-blast atomizer was discussed. Moreover, the influence of the interaction between two-stage counter swirling airflows on the characteristics of flow field was explained. The results show that with the increase in SNi, the axial length of the primary recirculation zone decreased, while the radial width increased. The starting position of primary recirculation zone (PRZ) moves forward with the increase in SNo. Reducing the sleeve angle β helps to form the primary recirculation zone. The results indicate that it is the transition of tangential velocity of airflow to radial velocity that promotes the formation of the PRZ. These results provide theoretical support for optimization of the flow field in swirl combustor.