AI Chat Paper
Note: Please note that the following content is generated by AMiner AI. SciOpen does not take any responsibility related to this content.
{{lang === 'zh_CN' ? '文章概述' : 'Summary'}}
{{lang === 'en_US' ? '中' : 'Eng'}}
Chat more with AI
Article Link
Collect
Show Outline
Outline
Show full outline
Hide outline
Outline
Show full outline
Hide outline
Open Access

A point cloud reconstruction method based on uncertainty feature enhancement for aerodynamic shape optimization

Junlin LIaYang ZHANGa( )Bo PANGaJunqiang BAIbJiakuan XUc
State Key Laboratory for Strength and Vibration of Mechanical Structures, Xi’an Jiaotong University, Xi’an 710049, China
Unmanned System Research Institute, Northwestern Polytechnical University, Xi’an 710072, China
School of Aeronautics, Northwestern Polytechnical University, Xi’an 710072, China

Peer review under responsibility of Editorial Committee of CJA.

Show Author Information

Abstract

The precision of shape representation and the dimensionality of the design space significantly influence the cost and outcomes of aerodynamic optimization. The design space can be represented more compactly by maintaining geometric precision while reducing dimensions, hence enhancing the cost-effectiveness of the optimization process. This research presents a new point cloud Autoencoder Based on Uncertainty Feature Enhancement (AE-BUFE) architecture, designed to attain efficient and precise generalized representations of 3D aircraft through uncertainty analysis of the deformation relationships among surface grid points. The deep learning architecture consists of two components: the uncertainty index-based feature enhancement module and the point cloud autoencoder module. It learns the shape features of the point cloud geometric representation to establish a low-dimensional latent space. To assess and evaluate the efficiency of the method, a comparison was conducted with the prevailing point cloud autoencoder architecture and the proper orthogonal decomposition linear dimensionality reduction method under conditions of complex shape deformation. The results show that the new architecture significantly improves the extraction effect of the low-dimensional latent space. Then, this paper developed the surrogate-based optimization framework based on the AE-BUFE parameterization method and completed a multi-objective aerodynamic optimization design for a wide-speed-range vehicle considering volume and moment constraints. While ensuring the take-off and landing performance, the aerodynamic performance is improved under transonic and hypersonic conditions, which verifies the efficiency and engineering practicability of this method.

References

【1】
【1】
 
 
Chinese Journal of Aeronautics

{{item.num}}

Comments on this article

Go to comment

< Back to all reports

Review Status: {{reviewData.commendedNum}} Commended , {{reviewData.revisionRequiredNum}} Revision Required , {{reviewData.notCommendedNum}} Not Commended Under Peer Review

Review Comment

Close
Close
Cite this article:
LI J, ZHANG Y, PANG B, et al. A point cloud reconstruction method based on uncertainty feature enhancement for aerodynamic shape optimization. Chinese Journal of Aeronautics, 2026, 39(6). https://doi.org/10.1016/j.cja.2025.103847

13

Views

0

Crossref

1

Web of Science

1

Scopus

0

CSCD

Received: 08 April 2025
Revised: 16 June 2025
Accepted: 27 July 2025
Published: 26 September 2025
© 2025 The Author(s). Chinese Society of Aeronautics and Astronautics.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).