Elastic-plastic buckling analysis of stiffened panel subjected to global bending in forming process

Author:

Zhou WenbinORCID,Shi ZhushengORCID,Li Yong,Rong Qi,Zeng Yuansong,Lin JianguoORCID

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference49 articles.

1. Integral Airframe Structures (IAS): Validated Feasibility Study of Integrally Stiffened Metallic Fuselage Panels for Reducing Manufacturing Costs;Munroe,2000

2. Creep-age forming AA2219 plates with different stiffener designs and pre-form age conditions: experimental and finite element studies;Lam;J. Mater. Process. Technol.,2015

3. An investigation of creep age forming of AA7B04 stiffened plates: experiment and FE modelling;Lyu;J. Manuf. Process.,2019

4. FEM equivalent model for press bend forming of aircraft integral panel;Yan;Trans. Nonferr. Met. Soc. China,2009

5. Prediction of fracture in press bend forming of aluminum alloy high-stiffener integral panels;Yan;Comput. Mater. Sci.,2011

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