Modelling Rotating Detonative Combustion Fueled by Partially Pre-vaporized n-Heptane Sprays
Majie Zhao, Huangwei Zhang

TL;DR
This study uses Eulerian-Lagrangian simulations to analyze how droplet size and fuel vapor ratios influence detonation behavior and droplet dynamics in rotating combustors fueled by partially vaporized n-heptane sprays.
Contribution
It provides new insights into the effects of droplet size and vaporization on detonation speed, fuel consumption, and combustion modes in RDC, highlighting the importance of droplet dynamics.
Findings
Smaller droplets vaporize completely around the detonation wave.
Detonation speed decreases with increasing droplet size.
Propagation speed increases with higher equivalence ratios.
Abstract
Eulerian-Lagrangian simulations are conducted for two-dimensional Rotating Detonative Combustion (RDC) fueled by partially prevaporized n-heptane sprays. The influences of droplet diameter and total equivalence ratio on detonation combustion and droplet dynamics are studied. It is found that small n-heptane droplets (e.g. 5 um) are completely vaporized around the detonation wave, while intermediate n-heptane droplets (e.g. 20 um) are consumed in or behind the detonation wave, with the escaped ones be continuously evaporated and deflagrated. The droplet distributions in the RDE combustor are significantly affected by the droplet evaporation behaviors. Mixed premixed and non-premixed combustion modes are seen in two-phase RDC. The detonated fuel fraction is high when the droplet diameters are small or large, reaching its minimal value with diameter being 20 um. The detonation propagation…
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Taxonomy
TopicsCombustion and Detonation Processes · Energetic Materials and Combustion · Rocket and propulsion systems research
