Damage prediction and failure mode analysis of composite aeroengine blade impacted by the breakstone
Author:
Funder
Aeronautical Science Foundation of China
Publisher
Springer Science and Business Media LLC
Link
https://link.springer.com/content/pdf/10.1007/s42401-024-00293-2.pdf
Reference20 articles.
1. Ma X-Q, Su Z-T (2020) Application progress of polymer matrix composites in civil turbofan aeroengine. J Mater Eng 48(10):48–59. https://doi.org/10.11868/j.issn.1001-4381.2020.000440
2. Sastry YBS, Kiros BG (2019) Impact analysis of compressor rotor blades of an aircraft engine. Front Struct Civ Eng 13(3):505–514. https://doi.org/10.1007/s11709-018-0493-3
3. Darla V, Ben BS, Srinadh KVS (2023) Performance based evaluation of the bond strength between aluminum hub and CFRP propeller blade profiles under cyclic aging environments. Int J Interact Des Manuf. https://doi.org/10.1007/s12008-023-01394-6
4. Uhlig K, Spickenheuer A, Bittrich L et al (2013) Development of a highly stressed bladed rotor made of a CFRP using the tailored fiber placement technology. Mech Compos Mater 49:201–210. https://doi.org/10.1007/s11029-013-9336-4
5. Kang YS, Park SW, Roh JS et al (2021) Computational investigation of effects of expanded metal foils on the lightning protection performance of a composite rotor blade. Int J Aeronaut Space Sci 22:203–221. https://doi.org/10.1007/s42405-020-00288-1
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