Inspection interval optimization for aircraft composite structures with dent and delamination damage
Author:
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Link
http://xplorestaging.ieee.org/ielx7/5971804/9367030/09369167.pdf?arnumber=9369167
Cited by 7 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. Experimental study of rotary ultrasonic high-quality hole processing of Glass Fiber Reinforced Plastic with a new diamond trepanning bit;Proceedings of the Institution of Mechanical Engineers, Part B: Journal of Engineering Manufacture;2023-08-16
2. Aircraft skin inspections: towards a new model for dent evaluation;Insight - Non-Destructive Testing and Condition Monitoring;2023-07-01
3. Improved Adaptive Compensation of Variant Fighter With Multiple Faults via Extended Observer;International Journal of Control, Automation and Systems;2023-05-26
4. Inspection Interval Optimization for Aircraft Composite Tail Wing Structure Using Numerical-Analysis-Based Approach;Mathematics;2022-10-17
5. The Effect of Internal Delamination Damage on the Tensile Strength of Aeronautical Composites;Acta Mechanica Solida Sinica;2022-06-22
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