# The research on active flow control method with vibration diaphragm on a NACA0012 airfoil at different stalled angles of attack

> Research article (Aerospace Science and Technology, 2017) · cited 30× · AI/ML

**Wikidata**: [openalex:W2657997908](https://www.wikidata.org/wiki/openalex:W2657997908)  
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