Numerical simulation of transpiration cooling for a high-speed boundary layer undergoing transition to turbulence (2023)

First Author: Sharma P
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.2023.108581

Publication URI: http://dx.doi.org/10.1016/j.ast.2023.108581

Type: Journal Article/Review

Parent Publication: Aerospace Science and Technology