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Keywords: Ducted tail rotor
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Journal Articles
Aircraft Engineering and Aerospace Technology: An International Journal (2018) 90 (2): 237–245.
Published: 05 March 2018
...Guo Zhong; Jun Huang; Mingxu Yi Purpose The purpose of this paper is to reduce the acoustic noise of helicopter ducted tail rotor. Design/methodology/approach To predict the noise accurately, a thin-body boundary element method (BEM)/Ffowcs Williams–Hawkings method is developed in this paper...
