Study of Film Cooling Effectiveness on a Double-Walled Effusion-Cooled Turbine Blade in a High-Speed Flow Using Pressure Sensitive Paint (2019)

First Author: Ngetich G
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/10.1115/gt2019-90545

Publication URI: http://dx.doi.org/10.1115/gt2019-90545

Type: Conference/Paper/Proceeding/Abstract