Methodology of substantive fatigue life valuation of composite components of aero structure-Reference-Cited by-同舟云学术

Methodology of substantive fatigue life valuation of composite components of aero structure

Published:2020-04-22 Issue:2 Volume:23 Page:59-71
ISSN:2542-0119
Container-title:Civil Aviation High Technologies
language:
Short-container-title:Naučn. vestn. MGTU GA

Author:

Strizhius V. E.¹

Affiliation:

1. NationalResearch University Moscow Aviation Institute

Publisher

Moscow State Institute of Civil Aviation

Subject

General Medicine

Reference16 articles.

1. Adam, T., Dickson, R.F., Fernando, G., Harris, B. and Reiter, H. (1986). The fatigue behavior of Kevlar/carbon hybrid composites. IMechE Conference Publications, Institute of Mechanical Engineers, no. 2, pp. 329-335.

2. Adam, T., Dickson, R.F., Jones, C.J., Reiter, H. and Harris, B. (1986). A power law fatigue damage model for fiber-reinforced plastic laminates. Proceedings of the Institution of Mechanical Engineers, Part C: Mechanical Engineering Science, vol. 200, issue 3, pp. 155-166. DOI: https://doi.org/10.1243/PIME_PROC_1986_200_111_02

3. Harris, B. (2003). A historical review of the fatigue behavior of fiber-reinforced plastics. Fatigue in composites, in B. Harris (Ed.). Woodhead Publishing Ltd and CRC Press LLC, pp. 3-35.

4. Nixon-Pearson, O.J. and Hallett, S.R. (2015). An investigation into the damage development and residual strengths of open-hole specimens in fatigue. Composites Part A: Applied Science and Manufacturing, vol. 69, pp. 266-278. DOI: https://doi.org/10.1016/j.compositesa.2014.11.013

5. Khan, A.I., Venkataraman, S. and Miller, I. (2018). Predicting fatigue damage of composites using strength degradation and cumulative damage model. Journal of Composites Science, vol. 2, issue 1. DOI: 10.3390/JCS2010009

Cited by 3 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. Numerical study of fatigue damage accumulation in composite wing panels of prospective supersonic transport aircraft;Aerospace Systems;2023-03-01

2. Features of fatigue and damage-tolerance tests of full-scale metal-composite aircraft structures;Industrial laboratory. Diagnostics of materials;2022-04-27

3. Designing of Thin Composite Panels with the Post-Buckling Behavior Considering Rigid Support and Loading with Shear Flows;Key Engineering Materials;2021-05