# Concept of self-excited unsteady flow control on a compressor blade and its preliminary proof by numerical simulation

> Research article (Aerospace Science and Technology, 2022) · cited 23× · AI/ML

**Wikidata**: [openalex:W4220807330](https://www.wikidata.org/wiki/openalex:W4220807330)  
**Source**: https://4ort.xyz/entity/concept-of-self-excited-unsteady-flow-control-on-a-compressor-blade-and-its-preliminary-proof-by-numerical-simulation
