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== Abstract ==
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 <jats:p>The article describes the impact of the gas turbine engine low-pressure turbine blade shroud shelf on the blade profile stress position. Attention is focused directly on the impact of the location of the gravity centre of the shroud shelf on blade stress distribution at the three most critical points of the profile. The paper describes the details of the calculation and the required expressions provided, as well as the results of the calculation example with clear graphical dependencies.
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Document type: Article
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== Full document ==
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<pdf>Media:Draft_Content_433664199-beopen671-9187-document.pdf</pdf>
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== Original document ==
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The different versions of the original document can be found in:
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* [https://content.sciendo.com/downloadpdf/journals/tae/7/1/article-p14.pdf https://content.sciendo.com/downloadpdf/journals/tae/7/1/article-p14.pdf] under the license https://creativecommons.org/licenses/by-nc-nd
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* [http://www.degruyter.com/view/j/tae.2019.7.issue-1/tae-2019-0002/tae-2019-0002.xml?format=INT http://www.degruyter.com/view/j/tae.2019.7.issue-1/tae-2019-0002/tae-2019-0002.xml?format=INT],
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: [https://doaj.org/toc/2255-9876 https://doaj.org/toc/2255-9876] under the license cc-by-nc-nd
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* [https://content.sciendo.com/view/journals/tae/7/1/article-p14.xml https://content.sciendo.com/view/journals/tae/7/1/article-p14.xml],
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: [http://www.degruyter.com/view/j/tae.2019.7.issue-1/tae-2019-0002/tae-2019-0002.pdf http://www.degruyter.com/view/j/tae.2019.7.issue-1/tae-2019-0002/tae-2019-0002.pdf],
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: [http://dx.doi.org/10.2478/tae-2019-0002 http://dx.doi.org/10.2478/tae-2019-0002]
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* [https://content.sciendo.com/view/journals/tae/7/1/article-p14.xml https://content.sciendo.com/view/journals/tae/7/1/article-p14.xml],
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: [https://academic.microsoft.com/#/detail/2938199432 https://academic.microsoft.com/#/detail/2938199432] under the license http://creativecommons.org/licenses/by/4.0
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Published on 01/01/2019

Volume 2019, 2019
DOI: 10.2478/tae-2019-0002
Licence: Other

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