Experimental investigation of the transonic shock-wave/boundary-layer interaction over a shock-generation bump (2020)
Attributed to:
Plasma Synthetic Jet Actuators for the Control of Transonic Shock Wave Boundary Layer Interaction
funded by
EPSRC
Abstract
No abstract provided
Bibliographic Information
Digital Object Identifier: http://dx.doi.org/10.1063/5.0018763
Publication URI: http://dx.doi.org/10.1063/5.0018763
Type: Journal Article/Review
Parent Publication: Physics of Fluids
Issue: 10