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Matematicheskoe modelirovanie, 2016, Volume 28, Number 2, Pages 53–64 (Mi mm3699)  

This article is cited in 9 scientific papers (total in 9 papers)

Study of different modes of fatigue fracture and durability estimation for compressor disc of gas turbine engine

N. G. Buragoa, A. B. Zhuravleva, I. S. Nikitinb, V. L. Yakushevb

a Ishlinsky Institute for Problems in Mechanics of RAS
b Institute for Computer Aided Design of RAS
Full-text PDF (491 kB) Citations (9)
References:
Abstract: Different criteria of the multiaxial fatigue fracture are studied for low-cycle fatigue (LCF) and their generalizations are proposed for very-high-cycle fatigue regime (VHCF). The procedure of the stress state calculation is described for the compressor disk of the gas turbine engine (GTE) in the flight cycle of loading and for the low-amplitude vibrations of the blades. The durability estimations of the disc operation are obtained for alternative mechanisms of fatigue LCF and VHCF using the calculated stress state and the models of multiaxial fatigue fracture. The results are compared with observed data during operation.
Keywords: low-cycle fatigue, very-high-cycle fatigue, durability estimation, stress concentration, centrifugal loading, high-frequency vibrations.
Funding agency Grant number
Russian Foundation for Basic Research 15-08-02392_а
Received: 29.06.2015
English version:
Mathematical Models and Computer Simulations, 2016, Volume 8, Issue 5, Pages 523–532
DOI: https://doi.org/10.1134/S2070048216050070
Bibliographic databases:
Document Type: Article
Language: Russian
Citation: N. G. Burago, A. B. Zhuravlev, I. S. Nikitin, V. L. Yakushev, “Study of different modes of fatigue fracture and durability estimation for compressor disc of gas turbine engine”, Matem. Mod., 28:2 (2016), 53–64; Math. Models Comput. Simul., 8:5 (2016), 523–532
Citation in format AMSBIB
\Bibitem{BurZhuNik16}
\by N.~G.~Burago, A.~B.~Zhuravlev, I.~S.~Nikitin, V.~L.~Yakushev
\paper Study of different modes of fatigue fracture and durability estimation for compressor disc of gas turbine engine
\jour Matem. Mod.
\yr 2016
\vol 28
\issue 2
\pages 53--64
\mathnet{http://mi.mathnet.ru/mm3699}
\elib{https://elibrary.ru/item.asp?id=25707624}
\transl
\jour Math. Models Comput. Simul.
\yr 2016
\vol 8
\issue 5
\pages 523--532
\crossref{https://doi.org/10.1134/S2070048216050070}
\scopus{https://www.scopus.com/record/display.url?origin=inward&eid=2-s2.0-84988014897}
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  • https://www.mathnet.ru/eng/mm/v28/i2/p53
  • This publication is cited in the following 9 articles:
    Citing articles in Google Scholar: Russian citations, English citations
    Related articles in Google Scholar: Russian articles, English articles
    Математическое моделирование
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    Abstract page:398
    Full-text PDF :224
    References:46
    First page:8
     
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