Influence of instability modes on cooling performance in hypersonic boundary layer with slot injection (2021)

First Author: Cerminara A
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/10.1016/j.ast.2020.106409

Publication URI: http://dx.doi.org/10.1016/j.ast.2020.106409

Type: Journal Article/Review

Parent Publication: Aerospace Science and Technology