Shear layer response to overmodulated acoustic perturbations (2023)
Attributed to:
Transpiration Cooling Systems for Jet Engine Turbines and Hypersonic Flight
funded by
EPSRC
Abstract
No abstract provided
Bibliographic Information
Digital Object Identifier: http://dx.doi.org/10.1063/5.0130336
Publication URI: http://dx.doi.org/10.1063/5.0130336
Type: Journal Article/Review
Parent Publication: Physics of Fluids
Issue: 1