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H

Hang Xiang

beihang university

H指数:6

被引数:177

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Enhancing thermal efficiency of micro gas turbine via data-driven integrated compressor-turbine aerothermodynamic optimization

通过数据驱动的压气机-涡轮气动热力学集成优化提升微型燃气轮机的热效率

Aerospace Science and Technology

IF5.8

2026-07-010

PRE

Integrated Surrogate Model-Based Approach for Aerodynamic Design Optimization of Three-Stage Axial Compressor in Gas Turbine Applications

基于集成代理模型的方法用于燃气轮机应用中三级轴流压缩机的气动设计优化

IF3.2

2026-03-030

OAAI

Enhancing aerodynamic performance and structural integrity of axial compressor through data-driven multi-objective optimization of strut wake flow

通过数据驱动的支柱尾流流场多目标优化提升轴流压气机的气动性能与结构完整性

Aerospace Science and Technology

IF5.8

2025-08-050

PRE

Enhancing aerodynamic and aeroelastic performance of axial compressor through multi-degree-of-freedom parameterization and data-driven multidisciplinary optimization

STRUCTURAL AND MULTIDISCIPLINARY OPTIMIZATION

IF4

2025-03-010

PRE

Adaptive boundary-constrained mesh deformation and data-driven aerodynamic optimization of compressor blade rows

PHYSICS OF FLUIDS

IF4.3

2025-02-110

PRE

Control parameter layout of compressor airfoils and adaptive optimization method for boundary extension

PHYSICS OF FLUIDS

IF4.3

2024-12-060

PRE

Prescreening surrogate-model-assisted multi-objective aerodynamic optimization design of highly loaded axial compressor in heavy-duty gas turbine

APPLIED THERMAL ENGINEERING

IF6.9

2024-10-011

PRE

Aerodynamic optimization of multi-stage axial turbine based on pre-screening strategy and directly manipulated free-form deformation

CASE STUDIES IN THERMAL ENGINEERING

IF6.4

2024-09-010

OAAI

Integrated optimization method for transonic turbine based on direct free-form deformation and prescreening differential evolutionary optimizer

IF9.4

2024-03-010

PRE

Aerodynamic modification and optimization of intermediate pressure compressor in marine intercooled recuperated gas turbine

船用中冷回热燃气轮机中压压气机气动改造及优化

CASE STUDIES IN THERMAL ENGINEERING

IF6.4

2023-05-014

OAAI

Aerothermodynamics optimal design of a multistage axial compressor in a gas turbine using directly manipulated free-form deformation

CASE STUDIES IN THERMAL ENGINEERING

IF6.4

2021-08-0121

OAAI

A surface parametric control and global optimization method for axial flow compressor blades

CHINESE JOURNAL OF AERONAUTICS

IF5.7

2019-07-0138

OAAI