摘要
描述了三维Ｅｕｌｅｒ方程数值模拟旋翼悬停流场的过程。欧拉方程的求解采用了网格中心有限体积法，五步Ｒｕｎｇｅ－Ｋｕｔｔａ时间推进格式。在没有建立尾迹模型的前提下，计算了两叶旋翼在亚、跨声速时的压强分布，并将计算结果与国外实验数据作了对比，二者吻合程度良好。
A numerical procedure is presented for calculating the flowfield over a lifting and nonlifting rotor in hover.The approach is to solve the inviscid compressible Euler equations in a rotor fixed frame of refrence using a finite volume method and Runge Kutta scheme.Without any wake model,the pressure distributions are presented for two bladed rotor,the theoretical results show good agreement with experiment data.
出处
《空气动力学学报》
CSCD
北大核心
1998年第3期282-287,共6页
Acta Aerodynamica Sinica
