Steady and unsteady aerodynamic loading of a NACA 16-616 aerofoil in a uniform flow (2022)
Attributed to:
Effect of Separation and Stall on Aerofoil Noise
funded by
EPSRC
Abstract
No abstract provided
Bibliographic Information
Digital Object Identifier: http://dx.doi.org/10.1017/aer.2022.66
Publication URI: http://dx.doi.org/10.1017/aer.2022.66
Type: Journal Article/Review
Parent Publication: The Aeronautical Journal
Issue: 1305