Simulating Low-Mach Compressible Flow at Large Prandtl Numbers with a High-Order Fully-Implicit All-Speed Flow Solver
ORAL
Abstract
We present a high-order, fully-implicit fluid dynamics solver for simulating very low-Mach compressible flow. The work is motivated by the development of large-scale simulations of high-explosive cookoff, which requires modeling multi-species/multi-phase reactive flow at high Peclet numbers.
The governing equations are discretized in space up to 5th-order with a reconstructed Discontinuous Galerkin method and integrated in time with L-stable fully implicit time discretization schemes. The resulting set of non-linear equations is converged using a robust physics-block based preconditioned Newton-Krylov solver, with the Jacobian-free version of the GMRES solver. We implement the low-Mach version of the AUSM+-up Riemann solver, which correctly mimics the pressure fluctuations of an incompressible flow solver in the asymptotic limit of small Mach number.
We demonstrate that our fully-implicit flow solver is able to robustly converge compressible flow calculations with Mach numbers less than 1.e-5. Furthermore, thin thermal boundary layers at high Prandtl numbers are easily resolved with a high-order discretization scheme.–
Presenters
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Brian Weston
Lawrence Livermore National Laboratory
Authors
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Brian Weston
Lawrence Livermore National Laboratory
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Amanda Braun
Purdue
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Robert Nourgaliev
Lawrence Livermore National Laboratory, Lawrence Livermore Natl Lab
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Jean-Pierre Delplanque
Univ of California - Davis