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C

Changpeng Cai

Jiangsu Province Key Laboratory of Aerospace Power System

H指数:11

被引数:342

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High-robustness acceleration control method for multi-combustion-chamber variable-cycle engine based on an improved Hopfield neural network

基于改进型Hopfield神经网络的变循环多燃烧室发动机高鲁棒性加速控制方法

Aerospace Science and Technology

IF5.8

2026-07-210

PRE

Thermodynamic Performance Online Optimization and Constraint Analysis of a Multi-Combustion Chamber Pre-Cooled Variable Cycle Engine

多燃烧室预冷变循环发动机的热力学性能在线优化与约束分析

International Journal of Aeronautical and Space Sciences

IF1.4

2025-12-010

PRE

Broad Flight Envelope Acceleration Control Method of Aero-Engine Based on Multiperiod Optimization Strategy

JOURNAL OF DYNAMIC SYSTEMS MEASUREMENT AND CONTROL-TRANSACTIONS OF THE ASME

IF1.3

2025-11-010

PRE

Research on low emission control method for ammonia and n-decane dual-fuel based pre-cooled high-flow variable cycle engine

基于氨和正癸烷双燃料预冷高流量变循环发动机的低排放控制方法研究

IF9.4

2025-10-150

PRE

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

带有冷却空气的自适应循环发动机的性能分析: 从推进性能，热力学效率，火用和红外特性

IF9.4

2024-11-011

PRE

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

APPLIED THERMAL ENGINEERING

IF6.9

2024-10-014

PRE

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

IF9.4

2024-09-011

PRE

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

燃料预冷多模式涡轮发动机模式过渡过程的热力学循环分析: 为什么？什么时候？怎么？

IF9.4

2024-03-013

PRE

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

APPLIED THERMAL ENGINEERING

IF6.9

2024-02-013

PRE

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

基于飞机/发动机综合优化设计的新型预冷超音速涡轮发动机热力学分析

IF9.4

2023-10-016

PRE

Performance assessment for a novel supersonic turbine engine with variable geometry and fuel precooled: From feasibility, exergy, thermoeconomic perspectives (vol 225, 120227, 2023)

APPLIED THERMAL ENGINEERING

IF6.9

2023-08-010

OAAI

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

涡轮冲压发动机模式转换过程中的推力增强控制程序设计

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2023-07-018

PRE

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

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2023-05-0113

PRE

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

APPLIED THERMAL ENGINEERING

IF6.9

2023-05-0118

PRE

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

通过可变几何调整提高商用涡扇发动机飞行任务性能的多个方面

IF9.4

2023-01-0111

PRE

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

CHINESE JOURNAL OF AERONAUTICS

IF5.7

2022-12-013

OAAI

Flow control of double bypass variable cycle engine in modal transition

双旁通变循环发动机模态转换时的流量控制

CHINESE JOURNAL OF AERONAUTICS

IF5.7

2022-10-0114

OAAI

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

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2022-09-0112

PRE

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

CHINESE JOURNAL OF AERONAUTICS

IF5.7

2022-08-013

OAAI

Numerical modeling on installed performance of turbofan engine with inlet ejector

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2021-05-0118

PREAI