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Xianjun Yu

bei hang university

H指数:20

被引数:1,156

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Experimental and numerical investigation of an integrated stator design strategy for corner separation control in aggressive compressor transition ducts

实验与数值研究：在激进压缩机过渡扩压器中用于控制角落分离的集成定子设计策略

Aerospace Science and Technology

IF5.8

2026-04-180

PRE

Experimental simulation of fouling effects in a four-stage low-speed axial compressor: Fouling distribution and performance changes

四级低速轴流压缩机的污垢效应实验模拟：污垢分布与性能变化

PHYSICS OF FLUIDS

IF4.3

2025-05-230

PRE

Breaking the geometry-performance tradeoff in compressor deviation modeling: Nested principal component analysis

CHINESE JOURNAL OF AERONAUTICS

IF5.7

2024-09-010

OAAI

Experimental study on the blade tip clearance sensitive effect in compressors with different loading levels

PHYSICS OF FLUIDS

IF4.3

2024-06-141

PRE

The effect of inlet profiles on the repeatability in the single-stage compressor

PHYSICS OF FLUIDS

IF4.3

2024-06-110

PRE

Experimental study on three-dimensional blade designs in an aggressive compressor transition duct

PHYSICS OF FLUIDS

IF4.3

2024-05-130

PRE

Development of a deviation package method for low-cost robust optimization in compressor blade design

CHINESE JOURNAL OF AERONAUTICS

IF5.7

2024-04-012

OAAI

New insights into component matching mechanism in the compression system of double bypass engine

PROPULSION AND POWER RESEARCH

IF6.3

2024-03-012

OAAI

Internal flow mechanism of an aggressive compressor transition duct

PHYSICS OF FLUIDS

IF4.3

2024-02-261

OA

Exploration of acceptable operating range for a compression system in a double bypass engine

CHINESE JOURNAL OF AERONAUTICS

IF5.7

2023-09-012

OAAI

Numerical and experimental study of bleed impact in multistage axial compressors

CHINESE JOURNAL OF AERONAUTICS

IF5.7

2023-02-014

OAAI

Method for utilizing PIV to investigate high curvature and acceleration boundary layer flows around the compressor blade leading edge

利用PIV研究压缩机叶片前缘周围高曲率和加速度边界层流动的方法

CHINESE JOURNAL OF AERONAUTICS

IF5.7

2022-12-014

OAAI

Using tandem blades to break loading limit of highly loaded axial compressors

CHINESE JOURNAL OF AERONAUTICS

IF5.7

2022-04-0128

OAAI

Nonlinear uncertainty quantification of the impact of geometric variability on compressor performance using an adjoint method

使用伴随方法对几何变化对压缩机性能的影响进行非线性不确定性量化

CHINESE JOURNAL OF AERONAUTICS

IF5.7

2022-02-0131

OAAI

The exploration of bypass matching limitation and mechanisms in adouble bypass engine compression system

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2021-12-0114

PRE

Experimental study of the Critical Incidence Phenomena in low speed compressor stators with both conventional and 3D blading designs

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2020-04-018

PREAI

On the mode transition of a double bypass variable cycle compression system

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2020-03-0123

PREAI

Control of compressor tip leakage flow using plasma actuation

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2019-03-0172

PREAI

Criteria for designing low-loss and wide operation range variable inlet guide vanes

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2018-09-0116

PREAI

Using wavelets to study spike-type compressor rotating stall inception

AEROSPACE SCIENCE AND TECHNOLOGY

IF5.8

2016-11-0129

PREAI