Zobrazeno 1 - 3
of 3
pro vyhledávání: '"Konstantin S. Fedechkin"'
Publikováno v:
Volume 2A: Turbomachinery.
The research is about the traditional approach in defects assessment, like damages in aviation engine blades and problems in their further use based on the defects analysis not in one blade or stage but in the multistage compressor as a whole. When a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a7382ca7ee02bff96bc0b53691dcfa8a
https://doi.org/10.1115/gt2020-16174
https://doi.org/10.1115/gt2020-16174
Autor:
Vyacheslav V. Bushmanov, Igor A. Leshenko, Olga V. Vinogradova, Gennady V. Kretinin, Kirill A. Vinogradov, Konstantin S. Fedechkin, Kseniia V. Otriakhina, Roman V. Khramin
Publikováno v:
Volume 2D: Turbomachinery.
A fan blade is a complicated object and obviously it is subjected to geometrical uncertainties from manufacture tolerances and other production deviations. In spite of all uncertainties a fan blade should provide stable aerodynamic efficiency and str
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c871add6f112309711a9e466258a4c92
https://doi.org/10.1115/gt2018-76816
https://doi.org/10.1115/gt2018-76816
Publikováno v:
11th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference.
Modern computer technologies now allow us to conduct rather complex mathematical calculations in a relatively short period of time. Thus, it has become possible to employ optimization methods in the design of various parts of aircraft engines, even w
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1d4c28269deaa40512aeeb6f438d7aa3
https://doi.org/10.2514/6.2006-6947
https://doi.org/10.2514/6.2006-6947