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Computational analysis of multi-fuel micro-gas turbine annular combustion chamber

Journal of thermal analysis and calorimetry, 2024-04, Vol.149 (8), p.3317-3329

2024

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Effect of pre-swirl nozzle closure modes on unsteady flow and heat transfer characteristics in a pre-swirl system of aero-engine

Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering, 2022-03, Vol.236 (4), p.685-703

2022

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Experimental and CFD analysis on the pressure ratio and entropy increment in a cover-plate pre-swirl system of gas turbine engine

Engineering applications of computational fluid mechanics, 2021-01, Vol.15 (1), p.476-489

2021

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Effects of blade surface roughness on compressor performance and tonal noise emission in a marine diesel engine turbocharger

Proceedings of the Institution of Mechanical Engineers. Part D, Journal of automobile engineering, 2020-12, Vol.234 (14), p.3476-3490

2020

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Effects of water ingestion on the tip clearance flow in compressor rotors

Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering, 2019-09, Vol.233 (11), p.4235-4246

2019

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A Passive Control Method of Hub Corner Stall in a 1.5-Stage Axial Compressor under Low-Speed Conditions

Energies (Basel), 2020-06, Vol.13 (11), p.2691

2020

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Theoretical and experimental evaluation of temperature drop and power consumption in a cover-plate pre-swirl system for gas turbine cooling

Case studies in thermal engineering, 2021-10, Vol.27, p.101221, Article 101221

2021

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Evaluation on the performance fluctuation after water ingestion for a turbofan engine compressor during flight descent

Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering, 2021-09, Vol.235 (12), p.1586-1604

2021

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Comprehensive evaluations of heat transfer performance with conjugate heat dissipation effect in high-speed rotating free-disk modeling of aero-engines

Fundamental research (Beijing), 2024-05, Vol.4 (3), p.611-623

2024

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Implementation of Three-Dimensional Inverse Design and Its Application to Improve the Compressor Performance

Energies (Basel), 2020-10, Vol.13 (20), p.5378

2020

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Numerical Analysis of High-Altitude Inlet Air on Boundary Layer Flow Loss in an Aero-Engine Compressor

Energies (Basel), 2020-08, Vol.13 (16), p.4155

2020

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A Diagnosis Method for the Compound Fault of Gearboxes Based on Multi-Feature and BP-AdaBoost

Symmetry (Basel), 2020-03, Vol.12 (3), p.461

2020

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Numerical Analysis of Aerodynamic Characteristics of Exhaust Passage with Consideration of Wet Steam Effect in a Supercritical Steam Turbine

Energies (Basel), 2020, Vol.13 (7), p.1560

2020

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Sensitivity Analysis of Multistage Compressor Characteristics Under the Spray Atomization Effect Using a CFD Model

Energies (Basel), 2019-01, Vol.12 (2), p.301

2019

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Optimum Tilt Angle of Flow Guide in Steam Turbine Exhaust Hood Considering the Effect of Last Stage Flow Field

Chinese journal of mechanical engineering, 2017-07, Vol.30 (4), p.866-875

English ed., 2017

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Sensitivity of air/mist non-equilibrium phase transition cooling to transient characteristics in a compressor of gas turbine

International journal of heat and mass transfer, 2019-07, Vol.137, p.882-894

2019

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Evaluation of mass injection cooling on flow and heat transfer characteristics for high-temperature inlet air in a MIPCC engine

International journal of heat and mass transfer, 2019-06, Vol.135, p.620-630

2019

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Comprehensive evaluations on performance and energy consumption of pre-swirl rotor–stator system in gas turbine engines

Energy conversion and management, 2021-09, Vol.244, p.114440, Article 114440

2021

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Evaluation and analysis of evaporation cooling on thermodynamic and pressure characteristics of intake air in a precooled turbine engine

International journal of hydrogen energy, 2021-07, Vol.46 (47), p.24410-24424

2021

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Prediction of the sealing flow effect on the temperature drop characteristics of a pre-swirl system in an aero-engine

Applied thermal engineering, 2021-05, Vol.189, p.116717, Article 116717

2021

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Conjugate heat transfer of impingement cooling using conical nozzles with different schemes in a film-cooled blade leading-edge

Applied thermal engineering, 2020-08, Vol.177, p.115491, Article 115491

2020

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Theoretical and experimental evaluations of pre-swirl rotor-stator system with inner seal bypass configuration for turbine performance improvement

Energy (Oxford), 2022-11, Vol.258, p.124760, Article 124760

2022

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Experimental investigations on flow and heat transfer characteristics in a high-speed rotor–stator disk cavity with axial throughflow

Applied thermal engineering, 2022-09, Vol.214, p.118630, Article 118630

2022

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Comprehensive investigations on fluid flow and heat transfer characteristics of a high-speed rotating turbine disk cavity system of aero-engine

International communications in heat and mass transfer, 2022-07, Vol.136, p.106170, Article 106170

2022

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Fluctuating characteristics of air-mist mixture flow with conjugate wall-film motion in a compressor of gas turbine

Applied thermal engineering, 2018-09, Vol.142, p.779-792

2018

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Computational analysis of multi-fuel micro-gas turbine annular combustion chamber

Effect of pre-swirl nozzle closure modes on unsteady flow and heat transfer characteristics in a pre-swirl system of aero-engine

Experimental and CFD analysis on the pressure ratio and entropy increment in a cover-plate pre-swirl system of gas turbine engine

Effects of blade surface roughness on compressor performance and tonal noise emission in a marine diesel engine turbocharger

Effects of water ingestion on the tip clearance flow in compressor rotors

A Passive Control Method of Hub Corner Stall in a 1.5-Stage Axial Compressor under Low-Speed Conditions

Theoretical and experimental evaluation of temperature drop and power consumption in a cover-plate pre-swirl system for gas turbine cooling

Evaluation on the performance fluctuation after water ingestion for a turbofan engine compressor during flight descent

Comprehensive evaluations of heat transfer performance with conjugate heat dissipation effect in high-speed rotating free-disk modeling of aero-engines

Implementation of Three-Dimensional Inverse Design and Its Application to Improve the Compressor Performance

Numerical Analysis of High-Altitude Inlet Air on Boundary Layer Flow Loss in an Aero-Engine Compressor

A Diagnosis Method for the Compound Fault of Gearboxes Based on Multi-Feature and BP-AdaBoost

Numerical Analysis of Aerodynamic Characteristics of Exhaust Passage with Consideration of Wet Steam Effect in a Supercritical Steam Turbine

Sensitivity Analysis of Multistage Compressor Characteristics Under the Spray Atomization Effect Using a CFD Model

Optimum Tilt Angle of Flow Guide in Steam Turbine Exhaust Hood Considering the Effect of Last Stage Flow Field

Sensitivity of air/mist non-equilibrium phase transition cooling to transient characteristics in a compressor of gas turbine

Evaluation of mass injection cooling on flow and heat transfer characteristics for high-temperature inlet air in a MIPCC engine

Comprehensive evaluations on performance and energy consumption of pre-swirl rotor–stator system in gas turbine engines

Evaluation and analysis of evaporation cooling on thermodynamic and pressure characteristics of intake air in a precooled turbine engine

Prediction of the sealing flow effect on the temperature drop characteristics of a pre-swirl system in an aero-engine

Conjugate heat transfer of impingement cooling using conical nozzles with different schemes in a film-cooled blade leading-edge

Theoretical and experimental evaluations of pre-swirl rotor-stator system with inner seal bypass configuration for turbine performance improvement

Experimental investigations on flow and heat transfer characteristics in a high-speed rotor–stator disk cavity with axial throughflow

Comprehensive investigations on fluid flow and heat transfer characteristics of a high-speed rotating turbine disk cavity system of aero-engine

Fluctuating characteristics of air-mist mixture flow with conjugate wall-film motion in a compressor of gas turbine

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