Xianjun Yu

发表

Experimental Investigation of the Flow Mechanisms and the Performance Change of a Highly Loaded Axial Compressor Stage with/without Stator Hub Clearance

Baojie Liu, Ying Qiu, Guangfeng An, 2019 .

Experimental investigation of the effect of rotor tip gaps on 3D separating flows inside the stator of a highly loaded compressor stage

Zhibo Zhang, Baojie Liu, Guangfeng An, 2016 .

The evolution of the flow topologies of 3D separations in the stator passage of an axial compressor stage

Zhibo Zhang, Baojie Liu, Xianjun Yu, 2013 .

Stereoscopic PIV measurement of unsteady flows in an axial compressor stage

Baojie Liu, Xianjun Yu, Bao-jie Liu, 2007 .

Application of SPIV in turbomachinery

Huijing Yuan, Baojie Liu, Xianjun Yu, 2006 .

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

Baojie Liu, Guangfeng An, Xianjun Yu, 2021, Aerospace Science and Technology.

Modeling of the double leakage and leakage spillage flows in axial flow compressors

Baojie Liu, H. Du, Xianjun Yu, 2014 .

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

Baojie Liu, Xianjun Yu, Hengtao Shi, 2018, Aerospace Science and Technology.

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

Baojie Liu, Xianjun Yu, Ruoyu Wang, 2020 .

Control of Corner Separation with Plasma Actuation in a High-Speed Compressor Cascade

Baojie Liu, Yun Wu, Ying-hong Li, 2017 .

Control of compressor tip leakage flow using plasma actuation

Baojie Liu, Yun Wu, Ying-hong Li, 2019, Aerospace Science and Technology.

Turbulence Models Assessment for Large-Scale Tip Vortices in an Axial Compressor Rotor

Baojie Liu, Xianjun Yu, Yangwei Liu, 2008 .

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

Qian ZHANG, Shenren XU, Xianjun YU, 2021, Chinese Journal of Aeronautics.

Evolution of the Tip Leakage Vortex in an Axial Compressor Rotor

Xianjun Yu, Hongwei Wang, Haokang Jiang, 2004 .

Relationship between the flow blockage of tip leakage vortex and its evolutionary procedures inside the rotor passage of a subsonic axial compressor

H. Du, Xianjun Yu, Zhibo Zhang, 2013 .

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

Guangfeng An, Xianjun Yu, Bao-jie Liu, 2022, Chinese Journal of Aeronautics.

Velocity Increment on Incidence Angle near the Leading Edge of the Compressor Cascade

Guangfeng An, Xianjun Yu, Bao-jie Liu, 2023, Aerospace.

Using wavelets to study spike-type compressor rotating stall inception

Yun Wu, Baojie Liu, Xianjun Yu, 2016 .

Development and Validation of a Novel Control-Volume Model for the Injection Flow in a Variable Cycle Engine

Guangfeng An, Xianjun Yu, Ruoyu Wang, 2022, Aerospace.

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

Guangfeng An, Xianjun Yu, Ruoyu Wang, 2023, Chinese Journal of Aeronautics.

Utilization of Zonal Method for Five-Hole Probe Measurements of Complex Axial Compressor Flows

Ying Qiu, Guangfeng An, Xianjun Yu, 2020 .

Analysis of Flow Characteristic of Transonic Tandem Rotor Airfoil and Its Optimization

Xianjun Yu, Yifei Wu, Yuan Tao, 2020, Applied Sciences.

A new method for rapid shock loss evaluation and reduction for the optimization design of a supersonic compressor cascade

Xianjun Yu, Hengtao Shi, Bao-jie Liu, 2018 .

An Integrated Throughflow Method for the Performance Analysis of Variable Cycle Compression Systems

Shaofeng Jia, Baojie Liu, Xianjun Yu, 2018 .

Quantitative evaluation of the unsteady behaviors of the tip leakage vortex in a subsonic axial compressor rotor

Guangfeng An, Xianjun Yu, Zhibo Zhang, 2016 .

A New Approach for Deviation Modeling in Compressors: Sensitivity-Correlated Principal Component Analysis

Baojie Liu, Guangfeng An, Xianjun Yu, 2023, Aerospace.

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

Baojie Liu, Guangfeng An, Xianjun Yu, 2023, Chinese Journal of Aeronautics.

A Novel Decomposition Method for Manufacture Variations and the Sensitivity Analysis on Compressor Blades

Baojie Liu, Guangfeng An, Xianjun Yu, 2022, Aerospace.

A Coupled Effect Model of Two-Position Local Geometric Deviations on Subsonic Blade Aerodynamic Performance

Baojie Liu, Guangfeng An, Xianjun Yu, 2020, Applied Sciences.

Application of MCST method to design the blade leading edge in axial compressors

Yuan Tao, Baojie Liu, Xianjun Yu, 2014 .

Influence Mechanisms of Manufacture Variations on Supersonic/Transonic Blade Aerodynamic Performances

Baojie Liu, Xianjun Yu, W. Shi, 2020, Turbomachinery.