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Quantifying Swirl Number Effects on Recirculation Zones and Vortex Dynamics in a Dual-Swirl Combustor

Swirl-stabilized combustors are central to gas turbine technology, where the swirl number critically determines flow structure and combustion stability. This work systematically investigates the isothermal flow in a dual-swirl combustor, focusing on two primary objectives: evaluating advanced turbul...

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Principais autores: Hafiz Ali Haider Sehole, Ghazanfar Mehdi, Rizwan Riaz, Absaar Ul Jabbar, Adnan Maqsood, Maria Grazia De Giorgi
Formato: Artigo
Idioma:Inglês
Publicado: MDPI AG 2025-12-01
Series:Energies
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Acceso en liña:https://www.mdpi.com/1996-1073/18/24/6568
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