Fatigue crack propagation for an aircraft compressor under input data variability

Author:

Giannella Venanzio,Sepe Raffaele,Citarella Roberto

Publisher

Elsevier BV

Subject

General Engineering,Energy Engineering and Power Technology

Cited by 6 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. Markov chain‐assisted stochastic model of crack growth rate;ZAMM - Journal of Applied Mathematics and Mechanics / Zeitschrift für Angewandte Mathematik und Mechanik;2023-12-10

2. Neural networks for fatigue crack propagation predictions in real-time under uncertainty;Computers & Structures;2023-11

3. Analysis of Fatigue Crack Propagation Law and Fault Characteristics on the Outer Edge of Aeroengine Compressor Disk;2023 Global Reliability and Prognostics and Health Management Conference (PHM-Hangzhou);2023-10-12

4. Aerodynamic performance improvement of the centrifugal compressor employing the elastic deformation theory;Journal of the Brazilian Society of Mechanical Sciences and Engineering;2023-10-06

5. Influence of 3D printing on compressor impeller fatigue crack propagation life;International Journal of Mechanical Sciences;2023-05

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