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The numerical analysis of aeroelastic behaviour of blade row of aviation engine fan

There presented the numerical analysis of oscillating blade row aeroelastic behaviour of aviation engine fan. The numerical method is based on solution of coupled problem of unsteady aerodynamics and blades elastic oscillations, equations in which are integrated with parallel-sequential information...

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Bibliographic Details
Main Authors: Гнесин, В. И., Колодяжная, Л. В., Кравченко, И. Ф., Меркулов, В. М., Шереметьев, А. В., Петров, А. В.
Format: Article
Language:Russian
Published: Інститут енергетичних машин і систем ім. А. М. Підгорного Національної академії наук України 2017
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Online Access:https://journals.uran.ua/jme/article/view/111548
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