Transition from complex strained state to simple one under non-proportional loading: comparison of various approaches

Object and purpose of research. This paper discusses ship structures. Its purpose is to compare the most common methods for transition from complex strained state to the simple one in calculations of fatigue strength under non-proportional loading. Materials and methods. This paper describes the met...

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Main Author: Anton R. Filatov
Format: Article
Language:English
Published: Krylov State Research Centre 2021-03-01
Series:Труды Крыловского государственного научного центра
Subjects:
Online Access:https://transactions-ksrc.ru/eng/archive/transition-from-complex-strained-state-to-simple-one-under-non-proportional-loading-comparison-of-va/
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spelling doaj-d7303346f5b94e10950ea82cfa3969d62021-03-24T08:56:17ZengKrylov State Research CentreТруды Крыловского государственного научного центра2542-23242618-82442021-03-013951424610.24937/2542-2324-2021-1-395-42-4625422324Transition from complex strained state to simple one under non-proportional loading: comparison of various approachesAnton R. Filatov0Krylov State Research CentreObject and purpose of research. This paper discusses ship structures. Its purpose is to compare the most common methods for transition from complex strained state to the simple one in calculations of fatigue strength under non-proportional loading. Materials and methods. This paper describes the method of absolute maximum principal stresses, the method of signed von Mises stresses, Sins method and critical-plane method. Main results. Analysis of time histories for design stresses obtained as per above-mentioned methods for the simplest examples of non-proportional loading. The comparison of these results was illustrated by a case study (loading of an icebreaker propulsion shaft). Conclusion. It is shown that, of all the methods discussed in this paper, only critical-plane method can fully take the loading process into account. None of the other methods can take into account the changes in orientation of principal stresses, so their results could be both somewhat too high and too low.https://transactions-ksrc.ru/eng/archive/transition-from-complex-strained-state-to-simple-one-under-non-proportional-loading-comparison-of-va/fatigue strengthnon-proportional loadingcomplex strained statecritical plane
collection DOAJ
language English
format Article
sources DOAJ
author Anton R. Filatov
spellingShingle Anton R. Filatov
Transition from complex strained state to simple one under non-proportional loading: comparison of various approaches
Труды Крыловского государственного научного центра
fatigue strength
non-proportional loading
complex strained state
critical plane
author_facet Anton R. Filatov
author_sort Anton R. Filatov
title Transition from complex strained state to simple one under non-proportional loading: comparison of various approaches
title_short Transition from complex strained state to simple one under non-proportional loading: comparison of various approaches
title_full Transition from complex strained state to simple one under non-proportional loading: comparison of various approaches
title_fullStr Transition from complex strained state to simple one under non-proportional loading: comparison of various approaches
title_full_unstemmed Transition from complex strained state to simple one under non-proportional loading: comparison of various approaches
title_sort transition from complex strained state to simple one under non-proportional loading: comparison of various approaches
publisher Krylov State Research Centre
series Труды Крыловского государственного научного центра
issn 2542-2324
2618-8244
publishDate 2021-03-01
description Object and purpose of research. This paper discusses ship structures. Its purpose is to compare the most common methods for transition from complex strained state to the simple one in calculations of fatigue strength under non-proportional loading. Materials and methods. This paper describes the method of absolute maximum principal stresses, the method of signed von Mises stresses, Sins method and critical-plane method. Main results. Analysis of time histories for design stresses obtained as per above-mentioned methods for the simplest examples of non-proportional loading. The comparison of these results was illustrated by a case study (loading of an icebreaker propulsion shaft). Conclusion. It is shown that, of all the methods discussed in this paper, only critical-plane method can fully take the loading process into account. None of the other methods can take into account the changes in orientation of principal stresses, so their results could be both somewhat too high and too low.
topic fatigue strength
non-proportional loading
complex strained state
critical plane
url https://transactions-ksrc.ru/eng/archive/transition-from-complex-strained-state-to-simple-one-under-non-proportional-loading-comparison-of-va/
work_keys_str_mv AT antonrfilatov transitionfromcomplexstrainedstatetosimpleoneundernonproportionalloadingcomparisonofvariousapproaches
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