Numerical Study on Aerodynamic and Noise Responses of Rotor with Ramp Increase in Collective Pitch Based on Time-Accurate Free-Wake Method

Research on helicopter transient maneuvering flight noise is a hotspot and challenging topic in the fields of helicopter design and application. A new time-accurate free-wake (TAFW) method and the Fowcs Williams-Hawkings (FW–H) equations are applied to analyze the aerodynamic and noise responses of...

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Bibliographic Details
Main Authors: Zhiyuan Hu, Runze Xia, Yongjie Shi, Guohua Xu
Format: Article
Language:English
Published: MDPI AG 2023-11-01
Series:Machines
Subjects:
Online Access:https://www.mdpi.com/2075-1702/11/11/1007