# Vortex dynamic mechanism of curved blade affecting flow loss in compressor cascade during corner stall process

> Research article (Aerospace Science and Technology, 2019) · cited 33× · AI/ML

**Wikidata**: [openalex:W2907624529](https://www.wikidata.org/wiki/openalex:W2907624529)  
**Source**: https://4ort.xyz/entity/vortex-dynamic-mechanism-of-curved-blade-affecting-flow-loss-in-compressor-cascade-during-corner-stall-process