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Методика прогноза остаточного ресурса вала несущего винта вертолета

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dc.contributor.author ВЛАДОВ, Михаил
dc.contributor.author ДОБРОВ, Дмитрий
dc.contributor.author УКРАИНЦЕВ, Даниил
dc.date.accessioned 2019-12-05T09:14:44Z
dc.date.available 2019-12-05T09:14:44Z
dc.date.issued 2012
dc.identifier.citation ВЛАДОВ, Михаил, ДОБРОВ, Дмитрий, УКРАИНЦЕВ, Даниил. Методика прогноза остаточного ресурса вала несущего винта вертолета. В: Telecommunication, Electronics and Informatics - ICTEI 2012: proc. of the 4th intern. conf., Technical University of Moldova, May 17-20, 2012. Chișinău, 2012, Vol. 2, pp. 297-302. ISBN 978-9975-45-082-9. en_US
dc.identifier.isbn 978-9975-45-082-9
dc.identifier.uri http://repository.utm.md/handle/5014/7273
dc.description.abstract In the report has described the technique of the helicopter rotor main draft shaft residual life prediction and has done description of the helicopter on-board rotor main draft shaft stress amplitude measurement and display system. en_US
dc.language.iso ru en_US
dc.publisher Tehnica UTM en_US
dc.rights Attribution-NonCommercial-NoDerivs 3.0 United States *
dc.rights.uri http://creativecommons.org/licenses/by-nc-nd/3.0/us/ *
dc.subject амплитуда напряжений вала несущего винта вертолета en_US
dc.subject измерение крутящего момента en_US
dc.subject прогноз остаточного ресурса вала en_US
dc.title Методика прогноза остаточного ресурса вала несущего винта вертолета en_US
dc.type Article en_US


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