Effect of the Cone Angle of the Impeller Hub of the Mixed Flow Compressor upon Performance Characteristics

650037

02/01/1965

Event
1965 International Automotive Engineering Congress and Exposition
Authors Abstract
Content
Experimental compressors, with impellers having impeller hub inclinations different from the rotation axis, and fitted with corresponding vaneless parallel walled diffusers, were tested. The results showed that the 45 deg impeller had the highest total pressure ratios and slip coefficients, especially at large weight flows. The 60 deg impeller had only slightly lower values, and the centrifugal impeller had the lowest.
Meta TagsDetails
DOI
https://doi.org/10.4271/650037
Pages
12
Citation
Watanabe, I., and Sakai, T., "Effect of the Cone Angle of the Impeller Hub of the Mixed Flow Compressor upon Performance Characteristics," SAE Technical Paper 650037, 1965, https://doi.org/10.4271/650037.
Additional Details
Publisher
Published
Feb 1, 1965
Product Code
650037
Content Type
Technical Paper
Language
English