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Flow control of double bypass variable cycle engine in modal transition

Chinese journal of aeronautics, 2022-10, Vol.35 (10), p.134-147

2022

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Maneuver control at high angle of attack based on real-time optimization of integrated aero-propulsion

Chinese journal of aeronautics, 2022-12, Vol.35 (12), p.173-188

2022

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Vector deflection stability control of aero-engine based on linear active disturbance rejection

Chinese journal of aeronautics, 2022-08, Vol.35 (8), p.221-235

2022

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Research on Optimal Control Method for Turbofan Engine Acceleration Process with Variable Air Bleed Considering High Pressure Turbine Guide Vane Life

International Journal of Aeronautical and Space Sciences, 2023, 24(2), , pp.475-487

2023

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Multi Combustor Turbine Engine Acceleration Process Control Law Design

Journal of dynamic systems, measurement, and control, 2024-10, p.1-15

2024

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Performance analysis of the adaptive cycle engine with cooling air: From propulsion performance, thermodynamic efficiency, exergy and infrared characteristics

Energy (Oxford), 2024-11, Vol.310, p.133215, Article 133215

2024

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Predictive control method for mode transition process of multi-mode turbine engine based on onboard adaptive composite model

Energy (Oxford), 2024-09, Vol.302, p.131748, Article 131748

2024

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Prediction of engine combustion chamber outlet temperature field based on deep Learning: Application in aero-engine life extension control

Applied thermal engineering, 2024-10, Vol.254, p.123911, Article 123911

2024

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Quasi One-Dimensional characteristic analysis of ejector nozzle for turbofan propulsion system

Applied thermal engineering, 2024-02, Vol.239, p.122112, Article 122112

2024

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Deep reinforcement learning method for turbofan engine acceleration optimization problem within full flight envelope

Aerospace science and technology, 2023-05, Vol.136, p.108228, Article 108228

2023

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Multiple aspects to flight mission performances improvement of commercial turbofan engine via variable geometry adjustment

Energy (Oxford), 2023-01, Vol.263, p.125693, Article 125693

2023

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Design of thrust augmentation control schedule during mode transition for turbo-ramjet engine

Aerospace science and technology, 2023-07, Vol.138, p.108352, Article 108352

2023

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Performance assessment for a novel supersonic turbine engine with variable geometry and fuel precooled: From feasibility, exergy, thermoeconomic perspectives

Applied thermal engineering, 2023-05, Vol.225, p.120227, Article 120227

2023

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Numerical modeling on installed performance of turbofan engine with inlet ejector

Aerospace science and technology, 2021-05, Vol.112, p.106590, Article 106590

2021

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Full-envelope acceleration control method of turbofan engine based on variable geometry compound adjustment

Aerospace science and technology, 2022-09, Vol.128, p.107748, Article 107748

2022

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A new method to improve the real-time performance of aero-engine component level model

International journal of turbo & jet-engines, 2023-03, Vol.40 (1), p.101-109

2023

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Thermodynamic analysis of a novel precooled supersonic turbine engine based on aircraft/engine integrated optimal design

Energy (Oxford), 2023-10, Vol.280, p.128161, Article 128161

2023

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Improved lumped parameter model for shear wall–frame structures with geometric and material nonlinearities

Journal of Building Engineering, 2024-08, Vol.91, p.109633, Article 109633

2024

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Thermodynamic cycle analysis of the fuel precooled multi-mode turbine engine mode transition process: Why? When? How?

Energy (Oxford), 2024-03, Vol.291, p.130358, Article 130358

2024

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An Optimal Speed Control Method of Multiple Turboshaft Engines Based on Sequence Shifting Control Algorithm

Journal of dynamic systems, measurement, and control, 2022-04, Vol.144 (4)

2022

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Corrigendum to “Performance assessment for a novel supersonic turbine engine with variable geometry and fuel precooled: From feasibility, exergy, thermoeconomic perspectives” [Appl. Therm. Eng. 225 (2023) 120227]

Applied thermal engineering, 2023-08, Vol.231, p.120851, Article 120851

2023

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A new method to improve the real-time performance of aero-engine component level model

International journal of turbo & jet-engines, 2020-10

2020

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Research on User Emotion Experience of Short Video Based on Cyclic Interaction Model

HCI International 2023 Posters, p.712-719

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GSENet:Global Semantic Enhancement Network for Lane Detection

Proceedings of the ... AAAI Conference on Artificial Intelligence, 2024, Vol.38 (13), p.15108-15116

2024

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Pt–CoP/C as an alternative PtRu/C catalyst for direct methanol fuel cells

Journal of materials chemistry. A, Materials for energy and sustainability, 2016, Vol.4 (47), p.18607-18613

2016

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Flow control of double bypass variable cycle engine in modal transition

Maneuver control at high angle of attack based on real-time optimization of integrated aero-propulsion

Vector deflection stability control of aero-engine based on linear active disturbance rejection

Research on Optimal Control Method for Turbofan Engine Acceleration Process with Variable Air Bleed Considering High Pressure Turbine Guide Vane Life

Multi Combustor Turbine Engine Acceleration Process Control Law Design

Performance analysis of the adaptive cycle engine with cooling air: From propulsion performance, thermodynamic efficiency, exergy and infrared characteristics

Predictive control method for mode transition process of multi-mode turbine engine based on onboard adaptive composite model

Prediction of engine combustion chamber outlet temperature field based on deep Learning: Application in aero-engine life extension control

Quasi One-Dimensional characteristic analysis of ejector nozzle for turbofan propulsion system

Deep reinforcement learning method for turbofan engine acceleration optimization problem within full flight envelope

Multiple aspects to flight mission performances improvement of commercial turbofan engine via variable geometry adjustment

Design of thrust augmentation control schedule during mode transition for turbo-ramjet engine

Performance assessment for a novel supersonic turbine engine with variable geometry and fuel precooled: From feasibility, exergy, thermoeconomic perspectives

Numerical modeling on installed performance of turbofan engine with inlet ejector

Full-envelope acceleration control method of turbofan engine based on variable geometry compound adjustment

A new method to improve the real-time performance of aero-engine component level model

Thermodynamic analysis of a novel precooled supersonic turbine engine based on aircraft/engine integrated optimal design

Improved lumped parameter model for shear wall–frame structures with geometric and material nonlinearities

Thermodynamic cycle analysis of the fuel precooled multi-mode turbine engine mode transition process: Why? When? How?

An Optimal Speed Control Method of Multiple Turboshaft Engines Based on Sequence Shifting Control Algorithm

Corrigendum to “Performance assessment for a novel supersonic turbine engine with variable geometry and fuel precooled: From feasibility, exergy, thermoeconomic perspectives” [Appl. Therm. Eng. 225 (2023) 120227]

A new method to improve the real-time performance of aero-engine component level model

Research on User Emotion Experience of Short Video Based on Cyclic Interaction Model

GSENet:Global Semantic Enhancement Network for Lane Detection

Pt–CoP/C as an alternative PtRu/C catalyst for direct methanol fuel cells

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