Research on the Nonlinear Structural Dynamic Characteristics of the Rigid Flexible Coupling Folding Wing Model for Aircraft

During the working process of the folding wing, there is not only a large-range rigid body motion but also a deformation motion of the flexible components.The problem of the rigid-flexible coupling of the structure is

Authors

Rui Yang
Shiyong Sun (ORCID: https://orcid.org/0000-0002-0435-1890)
Xin‐Qiang Lu

Institutions

Dalian University of Technology (CN)
Dalian University (CN)

Publication Details

Journal: Engineered Science
Published: 2025-01-01
DOI: https://doi.org/10.30919/es1586
Primary Topic: Structural Analysis and Optimization
Type: article
Field-Weighted Citation Impact: 0.00

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article

Research on the Nonlinear Structural Dynamic Characteristics of the Rigid Flexible Coupling Folding Wing Model for Aircraft

Rui Yang, Shiyong Sun, Xin‐Qiang Lu

Jan 1, 2025

Engineered Science

Structural Analysis and Optimization

article

Research on the Nonlinear Structural Dynamic Characteristics of the Rigid Flexible Coupling Folding Wing Model for Aircraft

Rui Yang, Shiyong Sun, Xin‐Qiang Lu

January 1, 2025article en

Abstract

Engineered Science

Dalian University of Technology (CN), Dalian University (CN)

Affordable and clean energy

Openalex Percentile: Top 85%

Structural Analysis and Optimization

DOI Open Access PDF OpenAlex

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Research on the Nonlinear Structural Dynamic Characteristics of the Rigid Flexible Coupling Folding Wing Model for Aircraft — Rui Yang, Shiyong Sun, et al. · Engineered Science (2025) | TGRS Research Map | TGRS