The Supersonic Axial-Flow Compressor (open access)

The Supersonic Axial-Flow Compressor

"An investigation has been made to explore the possibilities of axial-flow compressors operating with supersonic velocities into the blade rows. Preliminary calculations showed that very high pressure ratios across a stage, together with somewhat increased mass flows, were apparently possible with compressors which decelerated air through the speed of sound in their blading. The first phase of the investigation was the development of efficient supersonic diffusers to decelerate air through the speed of sound" (p. 473).
Date: March 8, 1946
Creator: Kantrowitz, Arthur
System: The UNT Digital Library