2015
DOI: 10.1002/fld.4000
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A simple hybrid finite volume solver for compressible turbulence

Abstract: SummaryA simple, explicit, hybrid finite volume method for simulating compressible turbulence is developed by combining a fourth‐order central scheme and a shock‐capturing simple low‐dissipation advection upstream splitting method. The total flux on each of the cell faces is computed as a weighted average of central/nondissipative and upwind/dissipative fluxes. The weights are determined using an unphysical oscillation sensor in addition to a more traditional discontinuity sensor used in earlier studies. Shock… Show more

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Cited by 8 publications
(5 citation statements)
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“…This test problem demonstrates the ability of higher-order methods to capture finer features in the flow with lower numerical diffusion. In particular, our third-order scheme is very competitive for this test problem: Chakravarthy et al (2015) show that they can capture the oscillations with 400 grid points (about 14 points per oscillation period, see their Figure 9), Derigs et al (2016) demonstrate good capturing with 256 points (about 9 per period, see their Figure 6), and with the DG-3 scheme, we obtain results comparable to this latter work with only 128 total grid points (i.e. 4 to 5 points per period, see the corresponding DG-3 = 7 line in Fig.…”
Section: Ldf Basis With Powell Termsmentioning
confidence: 96%
“…This test problem demonstrates the ability of higher-order methods to capture finer features in the flow with lower numerical diffusion. In particular, our third-order scheme is very competitive for this test problem: Chakravarthy et al (2015) show that they can capture the oscillations with 400 grid points (about 14 points per oscillation period, see their Figure 9), Derigs et al (2016) demonstrate good capturing with 256 points (about 9 per period, see their Figure 6), and with the DG-3 scheme, we obtain results comparable to this latter work with only 128 total grid points (i.e. 4 to 5 points per period, see the corresponding DG-3 = 7 line in Fig.…”
Section: Ldf Basis With Powell Termsmentioning
confidence: 96%
“…According to previous investigations, e.g. [73], a scheme is considered "acceptable" for capturing supersonic turbulence if the dynamics can be captured well with 400 cells. However, the entropy stable scheme is also able to resolve the dynamics of the flow with a much lower spatial resolution (the result used in Fig.…”
Section: Mhd Version Of Shu-osher Test (1d)mentioning
confidence: 99%
“…This is also a feature of hyperviscosity approaches (as seen in solutions for the Shu–Osher test). Note that the kink is reduced considerably when the RHLL scheme is used instead of the SLAU2 scheme .…”
Section: Resultsmentioning
confidence: 99%
“…Only pure WENO schemes are immune to this problem, but they have been deemed [9,10] too dissipative to capture turbulence accurately. 700 V. KALYANA CHAKRAVARTHY AND D. CHAKRABORTY A simple and effective way of dealing with numerical oscillations in hybrid, explicit finite volume schemes by basing the weights on a Gibbs phenomenon detector in addition to a more traditional discontinuity sensor was proposed earlier and studied using canonical problems [11]. The present work differs from an earlier study in two ways.…”
Section: Introductionmentioning
confidence: 92%
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