Modeling transient vibration-sound generation processes

Автор(и)

DOI:

https://doi.org/10.31713/MCIT.2020.03

Ключові слова:

helicopter’s noise.

Анотація

In this paper, a problem of sound generation of two-blade rotor sinusoidal shape during helicopter landing is solved. Near and far sound field characteristics have been calculated. A comparative analysis of obtained numerical results with results for Mach number 0.2<M<0.4 is given. In particular noticed, that for a low Mach’s number M<0.1 transitional mode can occurs, which produces a blade flutter as a result.

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Опубліковано

2020-10-22

Як цитувати

Lukianov, P. V. (2020). Modeling transient vibration-sound generation processes. Моделювання, керування та інформаційні технології, (4), 39–42. https://doi.org/10.31713/MCIT.2020.03

Номер

№ 4 (2020): Modeling, control and information technologies: Proceedings of IV International scientific and practical conference

Розділ

Mathematical modelling and computational methods