A mesoscopic modelling approach for direct numerical simulations of transition to turbulence in hypersonic flow with transpiration cooling (2020)

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.ijheatfluidflow.2020.108732

Publication URI: http://dx.doi.org/10.1016/j.ijheatfluidflow.2020.108732

Type: Journal Article/Review

Parent Publication: International Journal of Heat and Fluid Flow