Affiliation:
1. Harbin Institute of Technology, Harbin, People’s Republic of China
Abstract
This paper presents the results of the experimental investigations on the effects of leaned and curved blade of plane axial compressor cascade. The ink trace method has been used for the surface flow visualization. The five-hole probe measurements are performed at the cascade exit 12.5 percent chord downstream, and the static pressure distributions are measured on the endwalls and blade surfaces.
Publisher
American Society of Mechanical Engineers
Cited by
16 articles.
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