摘要
Ⅰ. INTRODUCTIONThe flow phenomena that exist in the advanced turbomachinery are extremely complex and propose a challenge to the engineers and scientists to improve the design procedure. The rapid progress of high speed and large capacity computers has encouraged the development of computational fluid dynamics that has had an increasingly important influence on turbomachinery blade design and analysis. Compared with the inviscid solver, the N.S.
基金
Project supported by the National Natural Science Foundation of China
