Crack growth rate and lifetime prediction for aviation gas turbine engine compressor disk based on nonlinear fracture mechanics parameters-Reference-Cited by-同舟云学术

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Crack growth rate and lifetime prediction for aviation gas turbine engine compressor disk based on nonlinear fracture mechanics parameters

Published:2019-10 Issue: Volume:103 Page:102313
ISSN:0167-8442
Container-title:Theoretical and Applied Fracture Mechanics
language:en
Short-container-title:Theoretical and Applied Fracture Mechanics

Author:

Shlyannikov V.N.,Ishtyryakov I.S.

Funder

Russian Science Foundation

Publisher

Elsevier BV

Subject

Applied Mathematics,Mechanical Engineering,Condensed Matter Physics,General Materials Science

Reference31 articles.

1. Evaluation of stress intensity factors for corner cracked turbine discs under arbitrary loading using finite element methods;Bell;Eng. Fract. Mech.,1989

2. Prediction of crack growth from bolt holes in a disk;Zhuang;Int. J. Fatigue,2000

3. Prediction of fatigue crack propagation lives of turbine discs with forging-induced initial cracks;Hou;Eng. Fract. Mech.,2014

4. Multilevel approach to lifetime assessment of steam turbines;Bnaszkiewicz;Int. J. Fatigue,2015

5. Structural integrity assessment of turbine disk on a plastic stress intensity factor basis;Shlyannikov;Int. J. Fatigue,2016

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