Summary of Research Progress in Supersonic Compressor Cascade
DOI:
https://doi.org/10.54097/hset.v49i.8534Keywords:
ultrasonic cascade, ultrasonic element, transonic /supersonic compressor, Unique intake Angle, Shock wave structure Shock wave/boundary layer interference.Abstract
In compressors, supersonic/transonic flow is a hot topic in today's research. Its development directly affects the performance and function of compressors. The main purpose of supersonic cascade research is to increase its tip velocity, so as to improve its power capacity and boost ratio. In this paper, important research achievements since 2017 are summarized in the following aspects: the working principle of ultrasonic elements, unique intake Angle, shock wave structure and boundary layer interference. At the same time, the most widely used design blade shapes are introduced. Finally, the future development is prospected.
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