A copy of this work was available on the public web and has been preserved in the Wayback Machine. The capture dates from 2017; you can also visit the original URL.
The file type is application/pdf.
Interface Effects Between a Moving Supersonic Blade Cascade and a Downstream Diffuser Cascade
1973
ASME 1973 International Gas Turbine Conference and Products Show
unpublished
Preserved Fulltext
Theoretical and experimental research conducted on a rotating supersonic blade cascade shows that absolute and relative velocities at rotor outlet are functions of the rotating cascade and the downstream diffuser cascade geometry, independently of the inlet mass flow rate. The radial maldistribution of the flow that results from this property of supersonic blade cascades is analyzed.
doi:10.1115/73-gt-23
fatcat:eka5qzq545eizgfb6iqztf2jfe