Load and Response Analysis of Tilting Rotor by Using Wake Bending Unsteady Dynamic Inflow Model
The traditional quasi-steady assumption model can not reflect the unsteady aerodynamic problems in the tilting of rotor. The CFD method based on the vortex theory can get better results, but it consumes a lot of computing resources. In this paper, the load and response of tilting rotor by using a wake bending unsteady dynamic inflow model were analyzed. Firstly, the effect of wake bending on induced inflow was investigated. Secondly, the six force coefficients and the transient response of blade flapping of rotor as a sinusoidal angular velocity tilting were calculated. The calculated results were analyzed to be physically reasonable.
tiltrotor dynamic inflow wake bending unsteady aerodynamics.
Hailong Yue Pinqi Xia
National Key Laboratory of Science and Technology on Rotorcraft Aeromechanics Nanjing University of Aeronautics and Astronautics Nanjing, Jiangsu, 210016, China
国际会议
南京
英文
1-6
2009-10-14（万方平台首次上网日期，不代表论文的发表时间）