摘要
WT5 'BZThis paper presents an unsteady and nonlinear wake model based on th e 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 use d in matrix prediction is removed. All of these enha ncements are aimed at the low speed flight phase and formulations for the induce d velocity field just in the TTP frame are derived. The corresponding FORTRAN pr ogram is tested and optimized for the real time applications on PCs.
基于被广泛应用的 Peters-He有限状态动态尾迹模型 ,本文提出了一种增强的非线性、非定常的旋翼尾迹模型 ,并混合王氏涡流理论建立了旋翼尾迹的旋转分量计算模型 (桨尖轨迹平面处 )。将原来的线性动态入流理论改造为非线性理论模型 ,并取消了计算影响系数矩阵中的小角度假设。增强后的诱导速度模型适合计算低速飞行状态下旋翼平面内诱导速度 ,理论计算结果和实验值吻合较好。经优化的 FORTRAN程序在常规单
