This postdoctoral project focuses on the numerical simulation of atomization and combustion of 
alternative liquid propellants for space propulsion.

The project comprises two main tasks: the numerical analysis of impinging jet atomization and the 
combustion modeling of the resulting spray.

Task 1 aims to validate advanced simulation tools, explore operating conditions, and analyze spray 
characteristics to guide experiments.

Task 2 aims to develop a combustion model for the alternative propellant; and to study the spray 
combustion using the characteristics obtained in Task 1.

The synergy between experiments and simulations at PPRIME will enable robust modeling and validation.

Candidates should hold a PhD in numerical fluid mechanics, with expertise in multiphase and/or reactive 
flows and interface tracking methods. Experience with Basilisk would be a strong asset.