A staggered pressure correction numerical scheme to compute a travelling reactive interface in a partially premixed mixture
D Grapsas, Rapha\`ele Herbin (AMU, I2M), J.-C Latch\'e (IRSN), Y, Nasseri (I2M)

TL;DR
This paper introduces a staggered pressure correction numerical scheme for simulating turbulent deflagrations with reactive interfaces, ensuring stability, conservation, and convergence in complex unstructured mesh computations.
Contribution
The paper presents a novel staggered, pressure correction scheme with a penalization approach for reactive flow simulation, maintaining stability and convergence properties.
Findings
Scheme preserves positivity of physical quantities.
Converges as chemical timescale tends to zero.
Achieves conservation of total energy in discrete form.
Abstract
We address in this paper a model for the simulation of turbulent deflagrations in industrial applications. The flow is governed by the Euler equations for a variable composition mixture and the combustion modelling is based on a phenomenological approach: the flame propagation is represented by the transport of the characteristic function of the burnt zone, where the chemical reaction is complete; outside this zone, the atmosphere remains in its fresh state. Numerically, we approximate this problem by a penalization-like approach, i.e. using a finite conversion rate with a characteristic time tending to zero with the space and time steps. The numerical scheme works on staggered, possibly unstructured, meshes. The time-marching algorithm is of segregated type, and consists in solving in a first step the chemical species mass balances and then, in a second step, mass, momentum and energy…
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Taxonomy
TopicsCombustion and flame dynamics · Computational Fluid Dynamics and Aerodynamics · Combustion and Detonation Processes
