Contribution a l’élaboration de la combustion supersonique avec modèle de cinétique chimique détaille sous Ansys fluent

Abstract

Our theme in this study is "Contributing to the development of supersonic combustion with a detailed chemical kinetic model under Ansys Fluent". We reviewed all the steps necessary for this study. We first reviewed the studies and the existing scramjet, an engine that includes this type of combustion. The mathematical and physical equations that help us study were then addressed. It was followed by the provision of information on general combustion and the faster-than-sound ingested combustion of hydrogen, showing the kinetic chemistry and how it works. Then we presented the geometry presented for the study and try to explain each of the steps we have taken. In the end, the results obtained were displayed.