01 — Propulsion research
Rotating Detonation Engine CFD study
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, LLNL H₂
- Solve time
- ~4 days, 4 cores
CONVERGE CFD, Fusion 360, Tecplot, ParaView, Python
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