arrow
返回

Aerodynamic shape optimization using a novel optimizer based on machine learning techniques

delete2019-03-01
delete126
PRE
AI
X
Xinghui Yan *
J
Jihong Zhu
匡
匡敏驰 (Minchi Kuang)
X
Xiangyang Wang
DOI:10.1016/j.ast.2019.02.003delete
delete原文链接
delete原文求助
delete分享
delete收藏
摘要

摘要

En 中文
Aerodynamic shape optimization is usually a loop of an optimization model, an optimizer and an evaluation workflow. A new optimizer is proposed and tested for a typical aerodynamic shape optimization of missile control surfaces with computational fluid dynamics (CFD). The new optimizer emphasizes the use of machine learning techniques, reinforcement learning and transfer learning, to improve performance and efficiency. Reinforcement learning is applied to extract the optimization experience from the semi-empirical method DATCOM using deep neural networks. Transfer learning is implemented to reuse the experience as priori knowledge in the CFD-based optimization by sharing neural network parameters. For the considered aerodynamic shape optimization problem of missile control surfaces, a remarkable reduction in the computational time has been accomplished. The new approach significantly decreases the required CFD calls by over 62.5%. Meanwhile, the time spent in the experience extraction and parameter transfer process is negligible. (C) 2019 Elsevier Masson SAS. All rights reserved.
Keyword:
Aerodynamic optimization
Reinforcement learning
Transfer learning
Computational fluid dynamics
AI总结

AI总结

对已上传原文的论文进行重点信息的提取,主要内容包括:简要概述、研究摘要、背景介绍、关键亮点、图文解析、展望与总结。

期刊

Aerospace Science and Technology 封面图
Aerospace Science and Technology
IF:
5.8
论文数:
1.0W
被引数:
3.0W

机构

T
tsinghua university
学者数:
11.9W
论文数: 10.0W
被引数: 137
引用论文

引用论文

Design and optimisation of a (FA)Q-learning-based HTTP adaptive streaming client
err2014-03-13
err62
errOAAI
errClaeys, Maxim; Latre, Steven; Famaey, Jeroen; Wu, Tingyao; Van Leekwijck, Werner; De Turck, Filip
err分享
err收藏
err分享
err收藏
err分享
err收藏
学者 查看更多内容