Modeling Thermodynamic Trends of Rotating Detonation Engines
James Koch, J. Nathan Kutz

TL;DR
This paper presents a modeling framework for rotating detonation engines that links wave dynamics and thermodynamic performance, accounting for geometric and chemical parameters, to better understand and optimize their operation.
Contribution
The authors develop a one-dimensional inviscid flow model that relates wave behavior to engine performance metrics without assuming specific wave topologies.
Findings
Wave separation influences propagation regimes and bifurcations.
Model estimates thermodynamic efficiency and work output based on process time scales.
Parameter variations affect wave behavior and engine performance.
Abstract
The formation of a number of co- and counter-rotating coherent combustion wave fronts is the hallmark feature of the Rotating Detonation Engine (RDE). The engineering implications of wave topology are not well understood nor quantified, especially with respect to parametric changes in combustor geometry, propellant chemistry, and injection and mixing schemes. In this article, a modeling framework that relates the time and spacial scales of the RDE to engineering performance metrics is developed and presented. The model is built under assumptions of backpressure-insensitivity and nominally choked gaseous propellant injection. The Euler equations of inviscid, compressible fluid flow in one dimension are adapted to model the combustion wave dynamics along the circumference of an annular-type rotating detonation engine. These adaptations provide the necessary mass and energy input and…
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