A Review of Intelligent Airfoil Aerodynamic Optimization Methods Based on Data-Driven Advanced Models
L Wang, H Zhang, C Wang, J Tao, X Lan, G Sun… - Mathematics, 2024 - mdpi.com
With the rapid development of artificial intelligence technology, data-driven advanced
models have provided new ideas and means for airfoil aerodynamic optimization. As the …
models have provided new ideas and means for airfoil aerodynamic optimization. As the …
An efficient robust aerodynamic design optimization method based on a multi-level hierarchical Kriging model and multi-fidelity expected improvement
Y Zhang, Z Han, W Song - Aerospace Science and Technology, 2024 - Elsevier
Robust aerodynamic design optimization (RADO) is developed to obtain aircraft designs
with insensitive aerodynamic performance. The uncertainties in manufacturing, operating …
with insensitive aerodynamic performance. The uncertainties in manufacturing, operating …
Robust optimization design of a blended wing-body drone considering influence of propulsion system
Y Wang, J Du, T Yang, J Zhou, B Wang, Y Shi… - Aerospace Science and …, 2025 - Elsevier
In contrast to conventional configurations, blended wing-body drones exhibit a pronounced
coupling between their aerodynamic and propulsion system. While this configuration …
coupling between their aerodynamic and propulsion system. While this configuration …
Manifold-guided multi-objective gradient algorithm combined with adjoint method for supersonic aircraft shape design
F Cao, Z Tang, C Zhu, X Zhao - Aerospace Science and Technology, 2024 - Elsevier
The aerodynamic design of supersonic aircraft necessitates the comprehensive
consideration of multiple conflicting design objectives and multi-disciplinary characteristics …
consideration of multiple conflicting design objectives and multi-disciplinary characteristics …
Aerodynamic shape optimization at low Reynolds number using multi-level hierarchical Kriging models
KS Rao, AN Abhilasha, A Das… - Optimization and …, 2024 - Springer
The aerodynamic performance characteristics of an unmanned aerial vehicle airfoil and
wing are optimized in the low Reynolds number regime using a variable-fidelity Multi-Level …
wing are optimized in the low Reynolds number regime using a variable-fidelity Multi-Level …
A novel accelerated convergence method for solving adjoint equations based on modal reduction
The efficiency of adjoint-based aerodynamic shape optimization depends critically on the
solution efficiency of adjoint equations. In this letter, we employ the Proper Orthogonal …
solution efficiency of adjoint equations. In this letter, we employ the Proper Orthogonal …
Optimization Design and Parameter Modeling for an Elliptic Shock Wave
H Li, Y Wang, S Xu, H Zhang - Journal of Aerospace Engineering, 2024 - ascelibrary.org
The elliptic shock wave has potential applications in the design of hypersonic inlets and
waveriders. In this study, an optimization design process and a mathematical model for an …
waveriders. In this study, an optimization design process and a mathematical model for an …
[HTML][HTML] 飞行器气动稳健优化设计方法研究进展
赵欢， 王摄昆， 高正红， 黄江涛 - 空气动力学学报, 2021 - pubs.cstam.org.cn
随着对现代飞行器性能需求的不断提高, 面向工程应用的先进气动外形设计方法要求能兼顾多
学科高性能和稳健性, 以突破传统设计方法设计的外形稳健性差, 难以实现工程应用的难题 …
学科高性能和稳健性, 以突破传统设计方法设计的外形稳健性差, 难以实现工程应用的难题 …