Multiblock residual-based compact schemes for the computation of complex turbomachinery flows

被引：6
|
作者：
Michel, B. [1 ]
Cinnella, P. [2 ]
Lerat, A. [2 ]
机构：
[1] Off Natl Etud & Rech Aerosp, Dept Simulat Numer Ecoulements & Aeroacoust, FR-92322 Chatillon, France
[2] Arts & Metiers ParisTech, Lab DynFluid, 151,Bd Hop, F-75013 Paris, France
来源：
INTERNATIONAL JOURNAL OF ENGINEERING SYSTEMS MODELLING AND SIMULATION | 2011年 / 3卷 / 1-2期
关键词：
compact scheme; multi-block grid; compressible flow; unsteady flow; turbomachinery;
D O I：
10.1504/IJESMS.2011.038745
中图分类号：
T [工业技术];
学科分类号：
08 ;
摘要：
A flexible multiblock implementation of second and third-order accurate residual-based compact (RBC) schemes is proposed and validated for turbomachinery flows of increasing complexity. Applications to complex transonic unsteady flows in turbomachinery show the advantages of using such schemes in terms of increased accuracy and better insight into the flow physics.
引用
收藏
页码：2 / 15
页数：14
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