A detailed modelling on spray atomisation and combustion of LOX/GCH4 in variable area pintle injector rocket engines

DOI10.1080/13647830.2021.1937702OpenAlexW3170879274MaRDI QIDQ5030797

Keonwoong Lee, Jaye Koo, Kanmaniraja Radhakrishnan

Publication date: 17 February 2022

Published in: Combustion Theory and Modelling (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1080/13647830.2021.1937702

zbMATH Keywords

Lagrangian approachvolume of fluid approachpintle injectorsheet formation and breakupspray and combustion characteristics

Mathematics Subject Classification ID

Fluid mechanics (76-XX) Thermodynamics and heat transfer (80Axx)

Cites Work

• Multiphysics simulations of rocket engine combustion
• A continuum method for modeling surface tension
• Large-eddy simulation of a turbulent piloted methane/air diffusion flame (Sandia flame D)
• Evaluation of equilibrium and non-equilibrium evaporation models for many-droplet gas-liquid flow simulations

This page was built for publication: A detailed modelling on spray atomisation and combustion of LOX/GCH4 in variable area pintle injector rocket engines