Influence of Spanwise and Streamwise Film Hole Spacing on Adiabatic Film Effectiveness for Effusion-Cooled Gas Turbine Blades (2021)

First Author: Courtis M
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/10.3390/ijtpp6030037

Publication URI: http://dx.doi.org/10.3390/ijtpp6030037

Type: Journal Article/Review

Parent Publication: International Journal of Turbomachinery, Propulsion and Power

Issue: 3