%0 Journal Article
%T Rotor Airload and Acoustics Prediction Based on CFD/CSD Coupling Method
%A Wang Liangquan
%A Xu Guohua
%A Shi Yongjie
%J 南京理工大学学报
%D 2018
%R 10.16356/j.1005-1120.2018.02.343
%X An advanced airload and noise prediction method based on computational fluid dynamics/computational structural dynamics (CFD/CSD) coupling for helicopter rotor has been developed in this paper. In the present method, Navier-Stokes equation is applied as the governing equation, and a moving overset grid system is generated in order to account for the blade motions in rotation, flapping and pitching. The blade structural analysis is based on 14-DOF Euler beam model, and the finite element discretization is conducted on Hamilton's variational principle and moderate deflection theory. Aerodynamic noise is calculated by Farassat 1A formula derived from FW-H equation. Using the developed method, numerical example of UH-60A is performed for aeroelastic loads calculation in a low-speed forward flight, and the calculated results are compared with both those from isolated CFD method and available experimental data. Then, rotor noise is emphatically calculated by CFD/CSD coupling method and compared with the isolated CFD method. The results show that the aerodynamic loads calculated from CFD/CSD method are more satisfactory than those from isolated CFD method, and the exclusion of blade structural deformation in rotor noise calculation may cause inaccurate results in low-speed forward flight state.
%K helicopter
%K rotor
%K airload
%K aerodynamic noise
%K computational fluid dynamics (CFD)
%K computational structural dynamics
%U http://tnuaa.nuaa.edu.cn/ch/reader/view_abstract.aspx?file_no=20180215&flag=1