Quantification of Cooled Film Thermal Protection Using Net Heat Flux Reduction within Transonic Environments

Considered are NHFR or net heat flux reduction data in order to illustrate and quantify turbulent thermal convection phenomena within a unique and intricate cooled film environment along the extremity end of a transonic turbine airfoil with a rim in the form of a squealer. Of particular focus are th...

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Veröffentlicht in:	Thermal engineering Jg. 72; H. 10; S. 802 - 816
Hauptverfasser:	Ligrani, P., Knox, N.
Format:	Journal Article
Sprache:	Englisch
Veröffentlicht:	Moscow Pleiades Publishing 01.10.2025 Springer Nature B.V
Schlagworte:	Airfoils Blade tips Boundary layers Combined-Cycle Power Plants and Their Auxiliary Equipment Convection cooling Cooling Engineering Engineering Thermodynamics Free convection Gas-Turbine Heat and Mass Transfer Heat flux Heat transfer Investigations Ratios Reynolds number Static pressure Steam-Turbine Temperature Thermal protection Turbines Velocity blowing ratio tip gap net heat flux reduction transonic flow cooled film squealer turbine airfoil
ISSN:	0040-6015, 1555-6301
Online-Zugang:	Volltext
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