Small gas turbine combustor experimental study: compliant metal/ceramic liner and performance evaluation... Liner temperature, performance, and exhaust emissions of the experimental combustor utilizing compliant metal/ceramic liners were determined and compared with three previously reported combustors that featured: (1) splash film-cooled liner walls; (2) transpiration cooled liner walls; and (3) counter-flow film cooled panels
Temperature mapping of air film-cooled thermal barrier coated surfaces using cr-doped gdalo3 phosphor thermography... In this presentation, temperature mapping by Cr:GdAlO3 based phosphor thermometry of air film-cooled TBC-coated surfaces is demonstrated for both scaled-up cooling hole geometries as well as for actual components in a burner rig test environment....
Advanced liner-cooling techniques for gas turbine combustors... Performance and liner cooling effectiveness of the experimental combustor configuration featuring counter-flow film-cooled panels is presented and compared with two previously reported combustors featuring: splash film-cooled liner walls; and transpiration cooled liner walls (Lamilloy)
Temperature mapping of air film-cooled thermal barrier coated surfaces using phosphor thermometry... Because decay time-based full-field phosphor thermometry is relatively immune to these effects, it can be applied advantageously to temperature mapping of air film-cooled TBC-coated surfaces....
