The application of support vector regression and virtual sample generation technique in the optimization design of transonic compressor
H Hu, Y Song, J Yu, Y Liu, F Chen - Aerospace Science and Technology, 2022 - Elsevier
With the development of artificial intelligence, machine learning technique has been applied
in turbomachinery optimization. However, the performance of a classic machine learning …
in turbomachinery optimization. However, the performance of a classic machine learning …
[HTML][HTML] A unified geometry parametrization method for turbomachinery blades
Turbomachinery design is increasingly carried out by means of automated workflows based
on high-fidelity physical models and optimization algorithms. The parametrization of the …
on high-fidelity physical models and optimization algorithms. The parametrization of the …
Aerodynamic and structural multidisciplinary optimization design method of fan rotors based on blade curvature constraints
Z Song, X Zheng, B Wang, K Zhou, RA Adjei - Aerospace Science and …, 2023 - Elsevier
The optimization design of the actual fan/compressor rotors is a multidisciplinary problem.
The aerodynamics and strength multidisciplinary optimization design of the fan/compressor …
The aerodynamics and strength multidisciplinary optimization design of the fan/compressor …
Integrated optimization method for transonic turbine based on direct free-form deformation and prescreening differential evolutionary optimizer
M Chen, J Chen, H Xiang, Y Liu, Y Guo - Energy, 2024 - Elsevier
With the increased load of turbine stages, shock waves and secondary flow influence the
performance of turbines more and more significantly. Aiming at improving the aerodynamic …
performance of turbines more and more significantly. Aiming at improving the aerodynamic …
Continuous adjoint‐based shape optimization of a turbomachinery stage using a 3D volumetric parameterization
XS Trompoukis, KT Tsiakas, VG Asouti… - … Methods in Fluids, 2023 - Wiley Online Library
This work presents a novel volumetric parameterization technique along with the continuous
adjoint method to support gradient‐based CFD shape optimization of turbomachinery …
adjoint method to support gradient‐based CFD shape optimization of turbomachinery …
[HTML][HTML] Integrated passage design based on extended free-form deformation and adjoint optimization
LI Xin, M Tongtong, W Li, Z Ling, JI Lucheng - Chinese Journal of …, 2023 - Elsevier
Inspired by the three-dimensional design of flow passages in turbomachinery, this study
proposes the concept of integrated passage design. The capability of adjoint method for …
proposes the concept of integrated passage design. The capability of adjoint method for …
Variable-fidelity expected improvement based efficient global optimization of expensive problems in presence of simulation failures and its parallelization
Y He, J Sun, P Song, X Wang - Aerospace Science and Technology, 2021 - Elsevier
To further alleviate the computational cost of single-fidelity efficient global optimization
(EGO) method, the variable-fidelity surrogate-based EGO method assisted by variable …
(EGO) method, the variable-fidelity surrogate-based EGO method assisted by variable …
Multidisciplinary design optimization for performance improvement of an axial flow fan using free-form deformation
This paper describes a multidisciplinary design optimization for performance improvement of
an electric-ducted fan rotor using free-form deformation (FFD) and data mining techniques. A …
an electric-ducted fan rotor using free-form deformation (FFD) and data mining techniques. A …
Machine learning enabled adaptive optimization of a transonic compressor rotor with precompression
In aerodynamic design, accurate and robust surrogate models are important to accelerate
computationally expensive computational fluid dynamics (CFD)-based optimization. In this …
computationally expensive computational fluid dynamics (CFD)-based optimization. In this …
Using shock control bumps to improve transonic fan/compressor blade performance
Shock control bumps can help to delay and weaken shocks, reducing loss generation and
shock-induced separation and delaying stall inception for transonic turbomachinery …
shock-induced separation and delaying stall inception for transonic turbomachinery …