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Autor:
A Vivek, T. N. Satish, G. Uma, Mangalanathan Umapathy, U. Chandrasekhar, G Kiran, A. N. V. Rao, SN Anagha
Publikováno v:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 234:342-360
Blade tip clearance is a critical engine health parameter measured on gas turbines. Increase in tip clearance results in decreased efficiency, whereas with decrease in clearance due to thermal and centrifugal loads, rotor blades might rub the engine
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::58b76d10c34f08336976393ec18ab634
https://doi.org/10.1177/0954410019865853
https://doi.org/10.1177/0954410019865853
