Numerical Investigation of the Aerodynamic and Acoustical Properties of a Shrouded Rotor

被引:7
作者
Abalakin, I. V. [1 ]
Anikin, V. A. [2 ]
Bakhvalov, P. A. [1 ]
Bobkov, V. G. [1 ]
Kozubskaya, T. K. [1 ]
机构
[1] Keldysh Inst Appl Math, Miusskaya Pl 4, Moscow 125047, Russia
[2] Design Off Kamov, Ul 8 Marta 8-A, Lubercy 111625, Moscow Oblast, Russia
关键词
shrouded rotor; viscous gas flows; aerodynamic forces; far field acoustics; numerical modeling; rotating coordinate system; EBR schemes; unstructured grids; FLIGHT; HOVER;
D O I
10.1134/S0015462816030145
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
The problem of shrouded rotor rotation is numerically solved basing on the Navier-Stokes equations in a noninertial coordinate system. The configuration considered is a model helicopter tail rotor. The calculations are performed using edge-based reconstruction (EBR) schemes on unstructured tetrahedral grids with the variables determined at gridpoints. The numerical results on the aerodynamic forces and the acoustic radiation intensity and direction in the far field are presented and analyzed.
引用
收藏
页码:419 / 433
页数:15
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