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26 April 2024 |
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Article overview
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Solid propellant combustion in the low Mach one-dimensional approximation: from an index-one differential-algebraic formulation to high-fidelity simulations through high-order time integration with adaptive time-stepping | Laurent François
; Joël Dupays
; Dmitry Davidenko
; Marc Massot
; | Date: |
6 Jul 2020 | Abstract: | An unsteady one-dimensional model of solid propellant combustion, based on a
low-Mach assumption, is presented and semi-discretised in space via a finite
volume scheme. The mathematical nature of this system is shown to be
differential-algebraic of index one. A high-fidelity numerical strategy with
stiffly accurate singly diagonally implicit Runge-Kutta methods is proposed,
and time adaptation is made possible using embedded schemes. High-order is
shown to be reached, while handling the constraints properly, both at the
interface and for the mass conservation in the gaseous flow field. Three
challenging test-cases are thoroughly investigated: ignition transients, growth
of combustion instabilities through a Hopf bifurcation leading to a limit cycle
periodic solution and the unsteady response of the system when detailed
gas-phase kinetics are included in the model. The method exhibits high
efficiency for all cases in terms of both computational time and accuracy
compared to first and second-order schemes traditionally used in the combustion
literature, where the time step adaptation is CFL-or variation-based. | Source: | arXiv, 2007.2538 | Services: | Forum | Review | PDF | Favorites |
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