Swirl number G : Angular momentum flux kgm 2 /s 2 G x : Axial momentum flux kgm/s 2 R : Burner exit radius mm sw : Mass flow rate through the swirler ports kg/s u sw : Tangential velocity at the swirler exit m/s A sw : Tangential injection area of the swirler m 2 ax : Density of axial inlet flow kg/m 3 A ax : Axial injection area m 2 u ax : Axial inlet velocity m/s
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Choi et al. (Wed,) studied this question.
www.synapsesocial.com/papers/69d8930e6c1944d70ce0423e — DOI: https://doi.org/10.15231/jksc.2025.30.4.058
Jinheon Choi
Tae‐Young Mun
Jaewon Chung
Journal of the Korean Society of Combustion
Korea University
Korea Institute of Energy Research
University of Science and Technology
Building similarity graph...
Analyzing shared references across papers
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