Acoustic Noise Prediction and Reduction Reasearch of Helicopter Ducted Tail Rotor
Chaopu Zhang, Mingxu Yi, Jun Huang, Liu Yang
Available Online September 2016.
- https://doi.org/10.2991/iccia-16.2016.36How to use a DOI?
- Acoustic noise; Noise reduction; ducted tail rotor.
- This research aims to study the acoustic noise prediction and reduction of helicopter ducted tail rotor. A thin-body BEM/FW-H method is developed to accurately predict the noise in this paper. It is a hybrid method combining computational aero acoustics with Boundary Element Method (BEM) and can be used efficiently to predict the propagation of sound wave in the duct. And two main geometry parameters are modified to investigate the noise reduction of ducted tail rotor by using the numerical prediction method. The acoustic performance of different modification tasks is discussed. These results verify the efficiency of design parameters modification to reduce acoustic noise of ducted tail rotor.
- Open Access
- This is an open access article distributed under the CC BY-NC license.
Cite this article
TY - CONF AU - Chaopu Zhang AU - Mingxu Yi AU - Jun Huang AU - Liu Yang PY - 2016/09 DA - 2016/09 TI - Acoustic Noise Prediction and Reduction Reasearch of Helicopter Ducted Tail Rotor BT - 2016 International Conference on Computer Engineering, Information Science & Application Technology (ICCIA 2016) PB - Atlantis Press SP - 193 EP - 199 SN - 2352-538X UR - https://doi.org/10.2991/iccia-16.2016.36 DO - https://doi.org/10.2991/iccia-16.2016.36 ID - Zhang2016/09 ER -