Modeling transient vibration-sound generation processes

Authors

DOI:

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

Keywords:

helicopter’s noise.

Abstract

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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Published

2020-10-22

Issue

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

Section

Mathematical, computer modeling and computational methods

How to Cite

Modeling transient vibration-sound generation processes. (2020). MCIT: Proceedings of International Scientific and Practical Conference, 4, 39-42. https://doi.org/10.31713/MCIT.2020.03