Rotating detonation engine CFD study
Senior research project, October 2025 to March 2026
An end-to-end design study of a small-scale hydrogen rotating detonation engine, carried from literature review to a working reacting-flow simulation. An RDE replaces the subsonic flame of a conventional combustor with a detonation wave travelling continuously around an annular channel.
I sized the combustor against the Bykovskii and Wolanski operability criteria, modelled it in Fusion 360, and built the reacting-flow case in CONVERGE CFD with detailed hydrogen chemistry, adaptive mesh refinement and periodic boundaries on an unwrapped annulus. The reference case reproduced a sustained rotating detonation wave, confirmed by front structure, periodic wrap-around without decay, and monitor-point pressure periodicity.
It is a demonstrated methodology and a qualitatively correct detonation, not a validated engine: wave speed was never compared against Chapman–Jouguet velocity, the cell-count cap ruled out a grid-convergence study, and the figures show that case rather than the custom geometry.
| Combustor bore | 75 mm |
|---|---|
| Annulus width | 2 mm |
| Chemistry | SAGE solver, LLNL hydrogen mechanism |
| Solve time | About 4 days on 4 cores |
Tools: CONVERGE CFD, Fusion 360, Tecplot, ParaView, Python.
Repository on GitHub










