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Guangfeng An

bei hang university

H指数:10

被引数:323

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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

A fast method for determining the operating domain of multistage compressors with variable stators

一种用于确定带可调静叶的多级压缩机运行域的快速方法

Aerospace Science and Technology

IF5.8

2026-02-100

PRE

A Loss Model System for Two-Dimensional Compressor Cascades of Modern Controlled Diffusion Airfoils

APPLIED SCIENCES-BASEL

IF2.5

2025-11-040

OAAI

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

Effects of speed ratio and flow rate on stall cell flow pattern and propagation in a counter-rotating axial compressor

转速比和流量对对转轴流压缩机失速团流型及传播的影响

PHYSICS OF FLUIDS

IF4.3

2025-04-180

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 and numerical investigation on rotating stall flow pattern in a counter-rotating axial compressor

PHYSICS OF FLUIDS

IF4.3

2024-07-310

PRE

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

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