2009
DOI: 10.1016/j.jcp.2009.02.027
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A method for avoiding the acoustic time step restriction in compressible flow

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Cited by 131 publications
(181 citation statements)
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“…Each figure also shows the resulting solution when solved using a traditional, fully explicit compressible flow solver with 3rd order accuracy in time and space, for comparison. We stress that the over-shoots near the shock front are a consequence of the semi-implicit discretization of the equations discussed in [21], as the implicit pressure system is centrally biased; to illustrate this point, we show in Figure 20: Density profile of a SOD shock tube at t = .15s, as generated by the scheme detailed in [21], using our new conservative semi-Lagrangian scheme and a CFL number of .5. We zoom in to the box [.725, .775] × [.…”
Section: Examplementioning
confidence: 99%
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“…Each figure also shows the resulting solution when solved using a traditional, fully explicit compressible flow solver with 3rd order accuracy in time and space, for comparison. We stress that the over-shoots near the shock front are a consequence of the semi-implicit discretization of the equations discussed in [21], as the implicit pressure system is centrally biased; to illustrate this point, we show in Figure 20: Density profile of a SOD shock tube at t = .15s, as generated by the scheme detailed in [21], using our new conservative semi-Lagrangian scheme and a CFL number of .5. We zoom in to the box [.725, .775] × [.…”
Section: Examplementioning
confidence: 99%
“…These are solved using the splitting proposed in [21]. Defining the state vector as U = (ρ, ρ u, E) T , the flux is split into its advective component, F 1 ( U ), and acoustic component F 2 ( U ):…”
Section: Compressible Flowmentioning
confidence: 99%
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