Qinglian Li

national university of defense technology

H指数:24

被引数:1,411

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Heat Transfer Characteristics Analysis of Spiral Regenerative Cooling Channel with Variable Helix Angle in LOX/CH4 Engine

变螺距角螺旋再生冷却通道在LOX/CH4发动机中的传热特性分析

Aerospace Science and Technology

IF5.8

2025-12-060

PRE

Research on cavitation and oscillation transition mechanism of adjustable cavitation Venturi tube

关于可调空化文丘里管空化与振荡转换机制的研究

Journal of Hydrodynamics

IF3.5

2025-10-230

PRE

Research on flow regulation and cavitation characteristics of adjustable venturis for liquid oxygen and methane

关于液氧和甲烷用可调文丘里管流量调节与空化特性的研究

Acta Astronautica

IF3.4

2025-08-070

PRE

Analyzing combustion performance of LOX/GCH4 pintle injector according to spray characteristics

根据喷雾特性分析LOX/GCH4喷嘴式喷注器的燃烧性能

Chinese Journal of Aeronautics

IF5.7

2025-07-240

OAAI

Experimental and numerical investigation of spray characteristics of gas-liquid swirl coaxial injectors

PHYSICS OF FLUIDS

IF4.3

2024-12-231

PRE

Experimental study on the penetration and evaporation characteristics of a liquid kerosene jet in the supersonic crossflow

PHYSICS OF FLUIDS

IF4.3

2024-07-233

PRE

Experiments investigation on atomization characteristics of a liquid jet in a supersonic combustor

PHYSICS OF FLUIDS

IF4.3

2024-04-251

PRE

Flow and spray characteristics of a gas-liquid pintle injector under backpressure environment

PHYSICS OF FLUIDS

IF4.3

2024-04-154

PRE

Study on the formation and maintenance mechanism of the stationary flame at the head of a LOX/GCH4 pintle injector element

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2024-02-015

PRE

Influence of helix angle on heat transfer characteristics of regenerative cooling in spiral channel

CASE STUDIES IN THERMAL ENGINEERING

IF6.4

2024-02-010

OAAI

Characteristics of penetration and distribution of a liquid jet in a divergent cavity-based combustor

CHINESE JOURNAL OF AERONAUTICS

IF5.7

2023-12-0118

OAAI

Experimental and theoretical study on the break phenomenon of self-pulsation for liquid-centered swirl coaxial injectors

液心旋流同轴喷射器自脉动破裂现象的实验和理论研究

zhejiang university science b

IF3.9

2022-03-073

PRE

Study on the heat transfer characteristics of regenerative cooling for LOX/LCH4 variable thrust rocket engine

CASE STUDIES IN THERMAL ENGINEERING

IF6.4

2021-12-0123

OAAI

Rapid and improved oral absorption of N-butylphthalide by sodium cholate-appended liposomes for efficient ischemic stroke therapy

通过添加胆酸钠的脂质体快速并改善N-丁苯酞的口服吸收，以有效治疗缺血性中风

DRUG DELIVERY

IF8.1

2021-11-1214

The break phenomenon of self-pulsation for liquid-centered swirl coaxial injectors

以液体为中心的旋流同轴喷射器的自脉动破坏现象

INTERNATIONAL JOURNAL OF MULTIPHASE FLOW

IF3.8

2021-09-019

PREAI

System scheme design of electric expander cycle for LOX/LCH4 variable thrust liquid rocket engine

ACTA ASTRONAUTICA

IF3.4

2021-09-0126

PREAI

Cross-sectional droplets distribution of a liquid jet in supersonic crossflow

ACTA ASTRONAUTICA

IF3.4

2021-09-0115

PREAI

Experimental and numerical investigation of cross-sectional structures of liquid jets in supersonic crossflow

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2020-08-0128

PREAI

System scheme design for LOX/LCH4 variable thrust liquid rocket engines using motor pump

ACTA ASTRONAUTICA

IF3.4

2020-06-0127

PREAI

Experimental investigation of nitrogen flow boiling heat transfer in a single mini-channel

zhejiang university science b

IF3.9

2020-02-2828

PRE

Qinglian Li

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