Output feedback control of flow separation over an aerofoil using plasma actuators (2018)
Attributed to:
Quiet aerofoils of the next generation
funded by
EPSRC
Abstract
No abstract provided
Bibliographic Information
Publication URI: https://api.elsevier.com/content/abstract/scopus_id/85055704610
Type: Journal Article/Review
Volume: 15
Parent Publication: International Journal of Numerical Analysis and Modeling
Issue: 6
ISSN: 17055105