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Yixin Yang

national university of defense technology - china

H指数:18

被引数:1,045

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Numerical investigation on the flow characteristics of shock trains in supersonic square-to-circular transition ducts

对超音速方形到圆形过渡风管中激波串流动特性的数值研究

Aerospace Science and Technology

IF5.8

2025-10-200

PRE

Weak heat release and complex combustion transitions in high-Mach scramjet combustor

高马赫数超燃冲压发动机燃烧室中的弱热释放和复杂的燃烧转捩

Applied Thermal Engineering

IF6.9

2025-09-140

PRE

Application of Mode Decomposition in Supersonic S-Shaped Pipes with Multiple Bending Angles

多弯曲角度超声速S形管道中模态分解的应用

IF2.8

2025-09-011

PRE

Turbulent boundary layer separation in supersonic S-shaped pipes with different flow turning angles

超声速S形管道中不同流动转向角度下的湍流边界层分离

PHYSICS OF FLUIDS

IF4.3

2025-05-200

PRE

On scale effect of supersonic combustion in axisymmetric combustor

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2024-12-011

PRE

Scenario driving cycle development by fine-granularity state identification and representative sequence excavation for application in energy management strategy

IF9.4

2024-12-010

PRE

Study on secondary motions in supersonic boundary layers of a bent pipe

PHYSICS OF FLUIDS

IF4.3

2024-09-251

PRE

Generation of inflow turbulence using an improved synthetic eddy method

PHYSICS OF FLUIDS

IF4.3

2024-08-060

PRE

Polyoxometalate Clusters Confined in Reduced Graphene Oxide Membranes for Effective Ion Sieving and Desalination

多金属氧酸盐簇限制在还原的氧化石墨烯膜中，用于有效的离子筛分和脱盐

ADVANCED SCIENCE

IF14.1

2024-06-170

OAAI

Investigation of multi-scale flow structures and combustion characteristics in a cavity-enhanced circular scramjet

COMBUSTION AND FLAME

IF6.2

2024-06-016

PRE

Molecular simulation and solubilities of (R,S)- and (S)-tetramisole hydrochloride in two binary solvents

JOURNAL OF MOLECULAR LIQUIDS

IF5.2

2024-06-0112

PRE

A multi-physics correction of the shear-stress transport turbulence model for supersonic flows

PHYSICS OF FLUIDS

IF4.3

2024-05-151

PRE

Effect of kerosene injection states on mixing and combustion characteristics in a cavity-based supersonic combustor

CHINESE JOURNAL OF AERONAUTICS

IF5.7

2024-04-0110

OAAI

Effect of kerosene injection states on mixing and combustion characteristics in supersonic combustor at high equivalent ratio

PHYSICS OF FLUIDS

IF4.3

2024-01-053

PRE

An alternative two-way coupled Euler-Lagrange scheme to model the performance of finite-size particle in supersonic flow

INTERNATIONAL JOURNAL OF MULTIPHASE FLOW

IF3.8

2024-01-015

OAAI

An improved flamelet/progress variable modeling in a hydrogen-fueled scramjet

INTERNATIONAL JOURNAL OF HYDROGEN ENERGY

IF8.3

2024-01-016

PRE

Large eddy simulation of supersonic flow in ducts with complex cross-sections

THEORETICAL AND APPLIED MECHANICS LETTERS

IF3.3

2023-11-011

OAAI

Effect of boundary layer thickness on supersonic combustion in a scramjet combustor

边界层厚度对超燃燃烧室超声速燃烧的影响

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2023-08-017

PRE

Numerical study of transverse jet mixing and combustion in a high-enthalpy supersonic crossflow with trace gases

PHYSICS OF FLUIDS

IF4.3

2023-03-2116

PRE

Modular polyoxometalate-intercalated layered double hydroxide membranes for molecular sieving and in situ regeneration

CELL REPORTS PHYSICAL SCIENCE

IF7.3

2022-12-018

OA