Breakup Mechanism of a Jet in the L-Shape Crossflow of a Gas Turbine Combustor

Experimental investigations are conducted to determine the mechanism and characteristics of a jet in an L-shape crossflow simulating the radial swirl injector of a lean premixed-prevaporized (LPP) combustor. To simplify the radial flow of the actual injector while ignoring the centrifugal effect, th...

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Bibliographic Details
Main Authors: Myeung Hwan Choi, Jeongwoo An, Jaye Koo
Format: Article
Language:English
Published: MDPI AG 2022-05-01
Series:Energies
Subjects:
Online Access:https://www.mdpi.com/1996-1073/15/9/3360