DNS of injection-induced transition in hypersonic flow over porous surfaces for transpiration cooling applications (2019)

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

Publication URI: https://api.elsevier.com/content/abstract/scopus_id/85084019627

Type: Other

Parent Publication: 11th International Symposium on Turbulence and Shear Flow Phenomena, TSFP 2019