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Effect of tip clearance variation in the transonic axial compressor of a miniature gas turbine at different Reynolds numbers

Aerospace science and technology, 2022-09, Vol.128, p.107793, Article 107793

2022

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Investigations on the unsteady flow mechanism of the high-throughflow fan with partial-height booster rotor

Proceedings of the Institution of Mechanical Engineers. Part A, Journal of power and energy, 2023-08, Vol.237 (5), p.939-952

2023

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The matching characteristics and flow mechanisms of partial-height booster rotor and fan rotor for a high-throughflow fan

Proceedings of the Institution of Mechanical Engineers. Part C, Journal of mechanical engineering science, 2022-12, Vol.236 (23), p.11240-11255

2022

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Effects of Bionic Leading Edge on the Aerodynamic Performance of a Compressor Cascade at a Low Reynolds Number

Journal of thermal science, 2024-07, Vol.33 (4), p.1272-1285

2024

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Numerical investigation of an aggressive s-shaped compressor transition duct with boundary layer suction

Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering, 2022-12, Vol.236 (16), p.3370-3386

2022

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A Phased Aerodynamic Optimization Method for Compressors Based on Multi-Degrees-of-Freedom Surface Parameterization

Journal of thermal science, 2021-11, Vol.30 (6), p.2071-2086

2021

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Research on aerodynamic optimization design method and flow mechanism of a high-subsonic compressor cascade

Engineering applications of computational fluid mechanics, 2022-12, Vol.16 (1), p.316-334

2022

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Effect of Non-Axisymmetric End Wall on a Highly Loaded Compressor Cascade in Multi-Conditions

Journal of thermal science, 2021-07, Vol.30 (4), p.1363-1375

2021

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Investigation on the Aerodynamic Performance and Flow Mechanism of Transonic Ultra-Highly Loaded Tandem-Rotor Stage

Aerospace, 2024-05, Vol.11 (5), p.389

2024

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Numerical investigation of a highly loaded centrifugal compressor stage with a tandem bladed impeller

Proceedings of the Institution of Mechanical Engineers. Part A, Journal of power and energy, 2018-05, Vol.232 (3), p.240-253

2018

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Flow Mechanism of a New Concept Transonic Tandem Fan Stage under the Design and Off-Design Conditions

Aerospace, 2022-11, Vol.9 (11), p.686

2022

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Vortex dynamics and entropy generation in separated transitional flow over a compressor blade at various incidence angles

Chinese journal of aeronautics, 2022-03, Vol.35 (3), p.42-52

2022

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High-pressure ratio centrifugal compressor with two different fishtail pipe diffuser configurations

Proceedings of the Institution of Mechanical Engineers. Part A, Journal of power and energy, 2018-11, Vol.232 (7), p.785-798

2018

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Influence of Variable-Geometry Adjustment on the Matching Characteristics of a Medium Variable Bypass Ratio Compression System

Aerospace, 2023-08, Vol.10 (8), p.707

2023

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Effects of surface roughness on the aerodynamic performance of a high subsonic compressor airfoil at low Reynolds number

Chinese journal of aeronautics, 2021-03, Vol.34 (3), p.71-81

2021

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The performance of a centrifugal compressor with a tandem impeller in off-design conditions

Proceedings of the Institution of Mechanical Engineers. Part A, Journal of power and energy, 2020-03, Vol.234 (2), p.156-172

2020

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Design Optimization of a Multistage Axial Flow Compressor Based on Full-Blade Surface Parameterization and Phased Strategy

International Journal of Aerospace Engineering, 2021-07, Vol.2021, p.1-25

2021

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Inducer/Exducer Matching Characteristics inside Tandem Impellers of a Highly Loaded Centrifugal Compressor

Journal of thermal science, 2020-08, Vol.29 (4), p.928-944

2020

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Optimal Design and Analysis of a High-Load Supersonic Compressor Based on a Surrogate Model

Aerospace, 2023-04, Vol.10 (4), p.364

2023

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Influence of Surface Roughness on a Highly Loaded Axial Compressor Stage Performance at Low Reynolds Number

International journal of aerospace engineering, 2021, Vol.2021, p.1-18

2021

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Optimization Design of a 2.5 Stage Highly Loaded Axial Compressor with a Bezier Surface Modeling Method

Applied sciences, 2020-06, Vol.10 (11), p.3860

2020

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Investigation of two pipe diffuser configurations for a compact centrifugal compressor

Proceedings of the Institution of Mechanical Engineers. Part G, Journal of aerospace engineering, 2018-03, Vol.232 (4), p.716-728

2018

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Numerical Investigation of the Bowed Stator Effects in a Transonic Fan at Low Reynolds Number

Journal of thermal science, 2017-01, Vol.26 (1), p.25-29

2017

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Numerical investigations of vortex dynamics and loss generation in the corner separation region of a high subsonic compressor blade

Physics of fluids (1994), 2023-02, Vol.35 (2)

2023

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Quasi-steady state mechanism study of a three bypass variable cycle engine fan based on variable outlet guide vane and variable area bypass injector

Energy (Oxford), 2024-10, Vol.306, p.132447, Article 132447

2024

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Effect of tip clearance variation in the transonic axial compressor of a miniature gas turbine at different Reynolds numbers

Investigations on the unsteady flow mechanism of the high-throughflow fan with partial-height booster rotor

The matching characteristics and flow mechanisms of partial-height booster rotor and fan rotor for a high-throughflow fan

Effects of Bionic Leading Edge on the Aerodynamic Performance of a Compressor Cascade at a Low Reynolds Number

Numerical investigation of an aggressive s-shaped compressor transition duct with boundary layer suction

A Phased Aerodynamic Optimization Method for Compressors Based on Multi-Degrees-of-Freedom Surface Parameterization

Research on aerodynamic optimization design method and flow mechanism of a high-subsonic compressor cascade

Effect of Non-Axisymmetric End Wall on a Highly Loaded Compressor Cascade in Multi-Conditions

Investigation on the Aerodynamic Performance and Flow Mechanism of Transonic Ultra-Highly Loaded Tandem-Rotor Stage

Numerical investigation of a highly loaded centrifugal compressor stage with a tandem bladed impeller

Flow Mechanism of a New Concept Transonic Tandem Fan Stage under the Design and Off-Design Conditions

Vortex dynamics and entropy generation in separated transitional flow over a compressor blade at various incidence angles

High-pressure ratio centrifugal compressor with two different fishtail pipe diffuser configurations

Influence of Variable-Geometry Adjustment on the Matching Characteristics of a Medium Variable Bypass Ratio Compression System

Effects of surface roughness on the aerodynamic performance of a high subsonic compressor airfoil at low Reynolds number

The performance of a centrifugal compressor with a tandem impeller in off-design conditions

Design Optimization of a Multistage Axial Flow Compressor Based on Full-Blade Surface Parameterization and Phased Strategy

Inducer/Exducer Matching Characteristics inside Tandem Impellers of a Highly Loaded Centrifugal Compressor

Optimal Design and Analysis of a High-Load Supersonic Compressor Based on a Surrogate Model

Influence of Surface Roughness on a Highly Loaded Axial Compressor Stage Performance at Low Reynolds Number

Optimization Design of a 2.5 Stage Highly Loaded Axial Compressor with a Bezier Surface Modeling Method

Investigation of two pipe diffuser configurations for a compact centrifugal compressor

Numerical Investigation of the Bowed Stator Effects in a Transonic Fan at Low Reynolds Number

Numerical investigations of vortex dynamics and loss generation in the corner separation region of a high subsonic compressor blade

Quasi-steady state mechanism study of a three bypass variable cycle engine fan based on variable outlet guide vane and variable area bypass injector

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