南京航空航天大学学报（英文版）2003，Vol.20Issue(1)：12-16,5.
一种适合飞行仿真应用的非定常非线性旋翼尾迹增强模型
ENHANCED UNSTEADY AND NONLINEAR ROTOR WAKE MODEL FOR REAL-TIME FLIGHT SIMULATION
孙传伟 1高正1
作者信息
- 1. 南京航空航天大学直升机技术研究所,南京,210016,中国
- 折叠
摘要
Abstract
This paper presents an unsteady and nonlinear wake model based on the widely used Peters-He finite state dynamic wake model with improvements. The swirl component in the tip-trace-plane (TTP) can be predicted, nonlinear items are added into the linear theory, and the old small angle assumption used in [L]-matrix prediction is removed. All of these enhancements are aimed at the low speed flight phase and formulations for the induced velocity field just in the TTP frame are derived. The corresponding FORTRAN program is tested and optimized for the real-time applications on PCs.关键词
直升机/旋翼/尾迹/动态入流Key words
helicopter/rotor/wake/dynamics inflow分类
航空航天引用本文复制引用
孙传伟,高正..一种适合飞行仿真应用的非定常非线性旋翼尾迹增强模型[J].南京航空航天大学学报（英文版）,2003,20(1):12-16,5.
