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Structure and stability of one-dimensional detonationsin ethylene-air mixtures
Authors:S. Yungster  K. Radhakrishnan
Affiliation:(1) Institute for Computational Mechanics in Propulsion, NASA Glenn Research Center, OH 44142 Cleveland, USA
Abstract:
The propagation of one-dimensional detonations in ethylene-air mixtures is investigated numerically by solving the one-dimensional Euler equations with detailed finite-rate chemistry. The numerical method is based on a second-order spatially accurate total-variation-diminishing scheme and a point implicit, first-order-accurate, time marching algorithm. The ethylene-air combustion is modeled with a 20-species, 36-step reaction mechanism. A multi-level, dynamically adaptive grid is utilized, in order to resolve the structure of the detonation. Parametric studies over an equivalence ratio range of $0.5 le phi le 3$ for different initial pressures and degrees of detonation overdrive demonstrate that the detonation is unstable for low degrees of overdrive, but the dynamics of wave propagation varies with fuel-air equivalence ratio. For equivalence ratios less than approximately 1.2 the detonation exhibits a short-period oscillatory mode, characterized by high-frequency, low-amplitude waves. Richer mixtures ($phi > 1.2$) exhibit a low-frequency mode that includes large fluctuations in the detonation wave speed. At high degrees of overdrive, stable detonation wave propagation is obtained. A modified McVey-Toong short-period wave-interaction theory is in excellent agreement with the numerical simulations.Received: 13 September 2004, Revised: 1 November 2004, Published online: 3 March 2005[/PUBLISHED]Correspondence to: S. Yungster
Keywords:Pulsating detonations  computational fluid dynamics  unsteady combustion
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