Wind-tunnel tests of synthetic jet control effects on airfoil flow separation

To find out the comprehensive principles of synthetic jet control effects on airfoil stall characteristics, fundamental contrastive wind-tunnel tests were conducted systematically. By using six-component balance, Particle Image Velocimetry (PIV) technology and boundary layer probe, the measurements...

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Detalles Bibliográficos
Autores principales: Zhao, Guoqing, Zhao, Qijun, Chen, Xi
Formato: Online Artículo Texto
Lenguaje:English
Publicado: Nature Publishing Group UK 2022
Materias:
Article
Acceso en línea:https://www.ncbi.nlm.nih.gov/pmc/articles/PMC9767908/
https://www.ncbi.nlm.nih.gov/pubmed/36539417
http://dx.doi.org/10.1038/s41598-022-19642-2

Internet

https://www.ncbi.nlm.nih.gov/pmc/articles/PMC9767908/
https://www.ncbi.nlm.nih.gov/pubmed/36539417
http://dx.doi.org/10.1038/s41598-022-19642-2

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