Aircraft Structure Paint Thickness and Lightning Swept Stroke Damages-Reference-Cited by-同舟云学术

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Aircraft Structure Paint Thickness and Lightning Swept Stroke Damages

Published:2013-09-17 Issue:2 Volume:6 Page:392-398
ISSN:1946-3901
Container-title:SAE International Journal of Aerospace
language:en
Short-container-title:SAE Int. J. Aerosp.

Author:

Moupfouma Fidele

Publisher

SAE International

Subject

Aerospace Engineering

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. Challenges and Future Recommendations for Lightning Strike Damage Assessments of Composites: Laboratory Testing and Predictive Modeling;Materials;2024-02-04

2. Performance of painted and non-painted non-woven nickel-coated carbon fibers for lightning strike protection of composite aircraft;Composites Part A: Applied Science and Manufacturing;2023-12

3. The Influence of Carbon Fiber Composite Specimen Design Parameters on Artificial Lightning Strike Current Dissipation and Material Thermal Damage;SAE International Journal of Aerospace;2023-04-29

4. Removal Mechanisms and Microstructure Characteristics of Laser Paint Stripping on Aircraft Skin Surface;Photonics;2023-01-16

5. Microwave cavity resonator sensor with an octagonal cross section for thickness measurement of coatings on carbon fibre composites;NDT & E International;2022-09

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