Compressor blade erosion modeling
- Authors: Gumerov A.V.1, Akmaletdinov R.G.2
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Affiliations:
- Scientific-and-production enterprise «Motor», Ufa
- Ufa state aviation technical university
- Issue: Vol 10, No 3-2 (2011): Special Issue
- Pages: 233-239
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/6817
- DOI: https://doi.org/10.18287/2541-7533-2011-0-3-2(27)-233-239
- ID: 6817
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Abstract
Jet engines are the basic type of engines in a civil and military aviation, used as main and forcings energy plant is in shipbuilding, energy, gas industry. A major requirement to the engines is high operating reliability. The design of processes of erosion by modern numerical complexes give new benefits for prognostication of the impermissible states of JE in exploitation, to apply on the stage of planning necessary and sufficient methods to protect engine details from erosion.
About the authors
A. V. Gumerov
Scientific-and-production enterprise «Motor», Ufa
Author for correspondence.
Email: fallenwarrior@yandex.ru
designer
Russian FederationR. G. Akmaletdinov
Ufa state aviation technical university
Email: akmar51@inbox.ru
candidate of technical sciences
head lecturer