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Wei Lin

jiangxi university of science & technology

H指数:20

被引数:1,290

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Correlation Mechanism Between Pressure Oscillation Characteristics of High-frequengy Tangential Combustion Instability in Hypergolic Propellants and Rotating Detonation

双组元自燃推进剂高频切向燃烧不稳定性的压力振荡特性与旋转爆震之间的关联机制

Acta Astronautica

IF3.4

2025-11-070

PRE

Directed transport of multiple deformable particles in time-oscillating potentials

在时变振荡势场中可变形粒子的定向输运

PHYSICAL REVIEW E

IF2.4

2025-11-060

PRE

The mixing enhancement mechanism and unsteady evaporation characteristics of the kerosene-air in the detonation combustor

IF7.5

2024-09-010

PRE

Early detection of thermoacoustic instability in an O2/CH4 single-injector rocket combustor using analysis of chaos and deep learning models

PHYSICS OF FLUIDS

IF4.3

2024-03-011

PRE

Experimental and numerical investigation of transverse combustion instability in a rectangle multi-injector rocket combustor

ACTA ASTRONAUTICA

IF3.4

2023-12-017

PRE

Analysis of self-excited transverse combustion instability in a rectangular model rocket combustor

PHYSICS OF FLUIDS

IF4.3

2022-04-0417

PRE

Mixing enhancement mechanism of combined H2-Water jets in supersonic crossflows in a combustor with an expanded section

INTERNATIONAL JOURNAL OF HYDROGEN ENERGY

IF8.3

2022-03-0112

PRE

Experimental and numerical study on multi-wavemodes of H2/O2rotating detonation combustor

INTERNATIONAL JOURNAL OF HYDROGEN ENERGY

IF8.3

2022-03-0113

PRE

Numerical study on atomization and evaporation characteristics of preheated kerosene jet in a rotating detonation scramjet combustor

旋转爆震超燃冲压发动机燃烧室预热煤油射流雾化和蒸发特性的数值研究

APPLIED THERMAL ENGINEERING

IF6.9

2022-02-0135

PRE

Experimental investigation on effects of injection distribution on combustion instability in a model rocket combustor

PHYSICS OF FLUIDS

IF4.3

2022-01-1012

PRE

Numerical simulation of single/double liquid jets in supersonic crossflows

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2022-01-0116

PRE

Analysis of spontaneous longitudinal combustion instability in an O2/CH4 single-injector rocket combustor

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2021-12-0121

PRE

Numerical Study of Effects of Backpressure on Self-Pulsation of a Liquid-Centred Swirl Coaxial Injector

背压对液心旋流同轴喷油器自脉动影响的数值研究

INTERNATIONAL JOURNAL OF MULTIPHASE FLOW

IF3.8

2021-06-019

PREAI

Simulation of a liquid jet in supersonic crossflow by a hybrid CLSVOF-LPT method

ACTA ASTRONAUTICA

IF3.4

2021-06-0124

PREAI

Numerical investigation on spray self-pulsation characteristics of a liquid-centered swirl coaxial injector

以液体为中心的旋流同轴喷射器喷雾自脉动特性的数值研究

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2021-05-0117

PREAI

Atomization of a liquid jet in supersonic crossflow in a combustion chamber with an expanded section

ACTA ASTRONAUTICA

IF3.4

2021-03-0137

PREAI

Structures of liquid jets in supersonic crossflows in a rectangular channel with an expansion section

PHYSICS OF FLUIDS

IF4.3

2020-11-1319

OAAI

Effects of air injection throat width on a non-premixed rotating detonation engine

ACTA ASTRONAUTICA

IF3.4

2019-06-0153

PREAI

Numerical investigation of a non-premixed hollow rotating detonation engine

INTERNATIONAL JOURNAL OF HYDROGEN ENERGY

IF8.3

2019-06-0147

PREAI

Plume flowfield and propulsive performance analysis of a rotating detonation engine

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2018-10-0143

PREAI