Numerical study on the effects of multiple inlet slot configurations on swirl cooling of a gas turbine blade leading edge
Author:
Publisher
Elsevier BV
Subject
Condensed Matter Physics,General Chemical Engineering,Atomic and Molecular Physics, and Optics
Reference32 articles.
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1. Numerical investigation on flow and heat transfer characteristics of impingement/swirl cooling structures in a turbine blade leading edge;International Journal of Heat and Fluid Flow;2024-09
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3. Investigations on Hot Air Anti-Icing Characteristics with Internal Jet-Induced Swirling Flow;Aerospace;2024-03-30
4. Experimental investigations on the heat transfer characteristic of impingement/swirl cooling structures inside turbine blade leading edge;International Communications in Heat and Mass Transfer;2024-01
5. Analysis of the Hydrodynamics of Swirling Flows in Direct-Flow Cyclones;Журнал прикладной химии;2023-12-15
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