Affiliation:
1. Office National d’Etudes et de Recherches Aérospatiales, Chatillon, France
Abstract
This paper describes a two dimensional unsteady calculation method which applies to the flow computation in two blade-rows having different angular speeds.
The Euler equations are solved using the classical predictor-corrector McCormack scheme. The program can be used in many cases involving time-dependent phenomena : mutual influence of two blade-rows, distortion problems, wake passage effects, aeroelasticity.
First, the computation program is described with a special importance being given to the boundary-conditions. Then, two calculation examples are given which allow one to evaluate the potential of this method for a detailed unsteady flow analysis.
Publisher
American Society of Mechanical Engineers
Cited by
9 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献