@inproceedings{3546eb00f76f4f6eb3edfa212fd578d9,
title = "Flame sustainability and thermal choking study of supersonic combustion of hydrogen, methane, and ethylene",
abstract = "Comparative numerical analysis is carried out for supersonic combustion of hydrogen, methane, and ethylene in a dual-mode scramjet engine with transverse fuel injection. The injection of three fuels is considered for a range of stagnation temperatures and jet-to-freestream momentum flux ratios. Turbulent supersonic combustion simulations are carried out using large-eddy simulations by using a recently developed interpolation-based flamelet/progress variable model. Flame sustainability is assessed based on the numerical results.",
author = "Wenhai Li and Foluso Ladeinde",
note = "Publisher Copyright: {\textcopyright} 2019, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.; AIAA Propulsion and Energy Forum and Exposition, 2019 ; Conference date: 19-08-2019 Through 22-08-2019",
year = "2019",
doi = "10.2514/6.2019-4272",
language = "English",
isbn = "9781624105906",
series = "AIAA Propulsion and Energy Forum and Exposition, 2019",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
booktitle = "AIAA Propulsion and Energy Forum and Exposition, 2019",
}