STUDY OF INTERACTIONS BETWEEN CLOSELY SPACED FILMS USED IN NOVEL HIGH POROSITY TURBINE BLADE COOLING DESIGNS (2023)
Attributed to:
Transpiration Cooling Systems for Jet Engine Turbines and Hypersonic Flight
funded by
EPSRC
Abstract
No abstract provided
Bibliographic Information
Type: Other
Parent Publication: European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, ETC
ISSN: 24104833 23130067