Calculation of the flow around a high-pressure turbine blade with cooling-jet injection from slots at the leading edge

DOI10.1023/A:1009964321807zbMath0944.76042OpenAlexW140272293MaRDI QIDQ1975851

G. Theodoridis, Wolfgang Rodi

Publication date: 20 September 2000

Published in: Flow, Turbulence and Combustion (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1023/a:1009964321807

zbMATH Keywords

leading-edge regionhigh-pressure turbine bladeisentropic Mach number distributionsslot cooling-jet injectionvectorized three-dimensional finite volume multi-block method

Mathematics Subject Classification ID

Finite volume methods applied to problems in fluid mechanics (76M12) General aerodynamics and subsonic flows (76G25)

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