Publisher
Springer Science and Business Media LLC
Subject
Mechanical Engineering,Mechanics of Materials,Safety, Risk, Reliability and Quality,General Materials Science
Reference39 articles.
1. D. Mangardich, F. Abrari, Z. Fawaz, Modeling crack growth of an aircraft engine high pressure compressor blade under combined HCF and LCF loading. Eng. Fract. Mech. 214, 474–486 (2019). https://doi.org/10.1016/j.engfracmech.2019.04.028
2. N.X. Hou, Z.X. Wen, Q.M. Yu, Z.F. Yue, Application of a combined high and low cycle fatigue life model on life prediction of SC blade. Int. J. Fatigue. 31, 616–619 (2009). https://doi.org/10.1016/j.ijfatigue.2008.03.021
3. J. Zhang, W.D. Liu, F.L. Liu et al., Analysis on tenon tooth cracks of a second stage high-pressure turbine blade. Eng. Fail. Anal. 141, 106681 (2022). https://doi.org/10.1016/j.engfailanal.2022.106681
4. S. Gurgen, M.C. Kus¸han, S.F. Diltemiz. Handbook of materials failure analysis with case studies from the aerospace and automotive industries, (chapter 13: Fatigue failure in aircraft structural components). pp. 266–269, ISBN: 978-0-12-800950-5. (2015)
5. H. Yan, P.D. Zhong, N.S. Xi, C.H. Tao, A case study of cracks in aero-engine compressor discs. Eng. Fail. Anal. 7, 181–188 (2000)