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Centrifugal Compressors The aerodynamic performance of impellers and diffusers of the large centrifugal compressor were studied
An experimental investigation to improve the stage efficiency through the use of vaned diffusers is presented Sixteen different vaned diffusers were tested
Aerodynamic performance at the stage level is reported for operation between 70 related to a new centrifugal compressor—the “High Efficiency Centrifugal
A transonic centrifugal compressor is optimized to improve the performance of the impeller by varying the geometry of blades and the meridional contour in
prediction of impeller aerodynamic performance for a single stage centrifugal compressor for which accurate test data is very difficult to obtain
Maximizing efficiency is the main goal in centrifugal compressor design Thus a computer code has been developed to optimize geometric and fluid dynamic