Numerical Simulation of Rotor–Wing Transient Interaction for a Tiltrotor in the Transition Mode

Tiltrotor aerodynamic interaction, especially in the transition mode, is a necessary consideration for tiltrotor aerodynamics, and structural design and optimization. Previous studies have paid much attention to the helicopter mode. However, due to the substantial complexity of the problem, only a s...

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Bibliographic Details
Main Authors: Zhenlong Wu, Can Li, Yihua Cao
Format: Article
Language:English
Published: MDPI AG 2019-01-01
Series:Mathematics
Subjects:
Online Access:https://www.mdpi.com/2227-7390/7/2/116