NASA NTRS · 19750000021
Computer program for definition of transonic axial-flow compressor blade rows
Abstract
Particular type of blade element used has two segments which have centerlines and surfaces described by constant change of angle with path distance on cone. Program is result of rework of earlier program to give major gains in accuracy, reliability and speed. It also covers more steps of overall compressor design procedure.
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Crouse, J. E.. 1975-04-01. Computer program for definition of transonic axial-flow compressor blade rows. https://ntrs.nasa.gov/citations/19750000021
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