Problem Statement
This report investigates the evaporation and combustion of n-heptane droplets injected into a subsonic crossflow of exhaust gases resulting from the stoichiometric combustion of air and Jet-A1 enriched with 20%wt hydrogen.
The analysis focuses on the trajectory and lifetime of a single droplet, initially considering pure evaporation and subsequently including combustion effects.
In the final section, a droplet population with diameters following a Gaussian distribution is analyzed under identical injection conditions.