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Research article

First published 2016-5

Effect of positioning errors of frames on fuselage panel assembly deformation

Weimiao Yan, Yunbo Bi, Mingjie Qiao

Advances in Mechanical Engineering

Free access

Research article

First published 2017-1

Optimal placement of measurement points on large aircraft fuselage panels in digital assembly

Yunbo Bi, Weimiao Yan, Yinglin Ke

Proceedings of the Institution of Mechanical Engineers,Part B: Journal of Engineering Manufacture

Retricted access

Review article

First published 2021-9

CFD-CSD method for coupled rotor-fuselage vibration analysis with free wake-panel coupled model

Siwen Wang, Jinglong Han, Haiwei Yun [...]

Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering

Retricted access

Research article

First published 2015-7

Multi load-transmitting device based support layout optimization for large fuselage panels in digital assembly

Yunbo Bi, Weimiao Yan, Yinglin Ke

Proceedings of the Institution of Mechanical Engineers,Part C: Journal of Mechanical Engineering Science

Retricted access

Research article

First published 2016-2

Impact of finite element idealisation on the prediction of welded fuselage stiffened panel buckling

T Ekmekyapar, A Murphy, D Quinn [...]

Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering

Retricted access

Research article

First published 2015-3

A coupled free-wake/panel method for rotor/fuselage/empennage aerodynamic interaction and helicopter trims

Yihua Cao, Shaojie Lv, Guozhi Li

Proceedings of the Institution of Mechanical Engineers,Part G: Journal of Aerospace Engineering

Retricted access

Research article

First published 2016-12

Optimal assembly of a skin panel onto the fuselage framework based on force control technology

Fengfeng Wu, Dongsheng Li, Baorui Du

Proceedings of the Institution of Mechanical Engineers,Part E: Journal of Process Mechanical Engineering

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Research article

First published 2013-6

Detecting and locating damage initiation and progression in full-scale sandwich composite fuselage panels using acoustic emission

Frank A Leone, Didem Ozevin, Jonathan Awerbuch [...]

Journal of Composite Materials

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Research article

First published 2002-02

Conceptual Design Principles for Non-Circular Pressurized Sandwich Fuselage Sections – a Design Study Based on a High-Order Sandwich Theory Formulation

Ole T. Thomsen, Jack R. Vinson

Journal of Composite Materials

Retricted access

Research article

First published 2025

Online monitoring method for geometric quality in fuselage panel riveting based on MBCNN-ViT

Huan Zhang, Yuhui Duan, Liang Cheng [...]

Proceedings of the Institution of Mechanical Engineers,Part B: Journal of Engineering Manufacture

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