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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Krylov State Research Centre
2021-03-01
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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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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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1724205190997868544 |