NASA NTRS · 19750003127
Transonic compressor technology advancements
Abstract
The highlights of the NASA program on transonic compressors are presented. Effects of blade shape and throat area on losses and flow range are discussed. Some effects of casing treatment on stall margin are presented. Results of tests with varying solidity are also presented. High Mach number, highly loaded stators are discussed and some results of stator hub slit suction are presented.
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Benser, W. A.. 1974-01-01. Transonic compressor technology advancements. https://ntrs.nasa.gov/citations/19750003127
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