您当前的位置：
首页 >
文章列表页 >
A Stiffness Modal Decomposition-Based Method for Assembly Deviation Prediction of Aeronautical Thin-Walled Structures
Research | 更新时间：2026-10-14

    • A Stiffness Modal Decomposition-Based Method for Assembly Deviation Prediction of Aeronautical Thin-Walled Structures

    • Aeronautical Manufacturing Technology   Vol. 69, Issue 19, (2026)

    • DOI：10.16080/j.issn1671-833x.26020042    

      CLC： V261.4

    • Received：09 February 2026，

      Revised：2026-02-26，

      Accepted：26 March 2026，

      Published：01 October 2026

    移动端阅览

  • JIANG Yibo, WEI Lei, CUI Zhanbo, et al. A stiffness modal decomposition-based method for assembly deviation prediction of aeronautical thin-walled structures[J]. Aeronautical Manufacturing Technology, 2026, 69(19): 26020042. DOI： 10.16080/j.issn1671-833x.26020042.

  •  
  •  

0

Views

3

下载量

0

CSCD

Alert me when the article has been cited
提交
Tools
Download
Export Citation
Share
Add to favorites
Add to my album

Related Articles

Optimization Method for Layout of Temporary Fasteners of Aircraft Composite Structure Assembly Pre-Joining
Analysis of Deformation and Localized Stress During Gap Compensation Joining Process of CFRP Panel Bolting
Methodology of Identifications and Tolerance Design of Machine Tools Crucial Geometric Error Elements
Evaluation of Uncertainty in Blade Parameter Measurement Based on Monte Carlo Method
Research Progress on Matrix Composition Regulation of SiC/SiC Composites

Related Author

GAO Shaowu
QU Zhengtao
AN Luling
ZHAO Cong
ZHOU Laishui
WU Yuetao
MENG Qingxun
LIU Tianpei

Related Institution

Nanjing University of Aeronautics and Astronautics
Innovation Center of Jiangsu Province for Advanced Composite Technology and Equipment
Shenyang Aerospace University
AVIC Shenyang Aircraft Industry (Group) Co., Ltd.
Southwest Petroleum University
0