Modelling bird impacts on an aircraft wing – Part 1: Material modelling of the fibre metal laminate leading edge material with continuum damage mechanics-Reference-Cited by-同舟云学术

Modelling bird impacts on an aircraft wing – Part 1: Material modelling of the fibre metal laminate leading edge material with continuum damage mechanics

Published:2005-01 Issue:1 Volume:10 Page:41-49
ISSN:1358-8265
Container-title:International Journal of Crashworthiness
language:en
Short-container-title:International Journal of Crashworthiness

Author:

McCarthy M A,Xiao J R,Petrinic N,Kamoulakos A,Melito V

Publisher

Informa UK Limited

Subject

Industrial and Manufacturing Engineering,Mechanical Engineering,Transportation

Link

http://www.tandfonline.com/doi/pdf/10.1533/ijcr.2005.0324

Reference16 articles.

1. Impact loading on fibre metal laminates

2. Towards application of fibre metal laminates in large aircraft

3. Development of fibre metal laminates for advanced aerospace structures

4. Impact properties of Fibre Metal Laminates

5. The Effect of Strain-Rate Upon the Tensile Deformation of Materials

Cited by 18 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Application of Macro Element Method (MEM) for faster automotive crash safety design during concept stage;International Journal of Crashworthiness;2023-09-21

2. A developed energy-dependent model for studying thermal shock damage and phase transition of composite reinforced panel subjected to lightning strike;European Journal of Mechanics - A/Solids;2021-01

3. Structural and CFD analysis of an airfoil subjected to bird strike;European Journal of Mechanics - B/Fluids;2020-11

4. Material parametric optimisation of wing leading edge profile against soft body impact;International Journal of Crashworthiness;2020-10-29

5. Simulation of High Velocity Impact on Composite Structures - Model Implementation and Validation;Applied Composite Materials;2016-05-16