Goffart et al 2022a - Revision history

Ngoffart at 09:31, 6 December 2022

2022-12-06T09:31:58Z

Move page script: Move page script moved page Goffart et al 1970a to Goffart et al 2022a

2022-11-25T15:06:13Z

Move page script moved page Goffart et al 1970a to Goffart et al 2022a

JSanchez: JSanchez moved page Draft Sanchez Pinedo 983382402 to Goffart et al 1970a

2022-11-22T13:56:52Z

JSanchez moved page Draft Sanchez Pinedo 983382402 to Goffart et al 1970a

JSanchez at 13:56, 22 November 2022

2022-11-22T13:56:44Z

JSanchez at 13:56, 22 November 2022

2022-11-22T13:56:42Z

JSanchez at 13:56, 22 November 2022

2022-11-22T13:56:40Z

JSanchez: Created blank page

2022-11-22T13:56:38Z

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 In this work, a high-order implicit large-eddy simulation of an oblique shockwave/boundary layer interaction at Mach 2.3 is performed. The high-order solver is based on the flux reconstruction method, allowing an arbitrary order of accuracy. A particular attention is paid to the shock-capturing technique which consists in a combination of a Laplacian artificial viscosity with the Ducros sensor. The ability of such a solver to accurately predict the flow features is assessed on both steady and unsteady fields. In particular, the typical lowfrequency motion of the reflected shock is reproduced. The shock-capturing methodology is proven to be efficient at resolving the shocks without damping the turbulence in the boundary layer. The results obtained give confidence in this solver to study in more details the shockwave/boundary layer interaction phenomenon and future work is focused on the analysis of the oscillatory turbulent field in the interaction region.
-== Abstract ==
+<!-- == Abstract == -->
-<pdf>Media:Draft_Sanchez Pinedo_983382402589_abstract.pdf</pdf>
+<!-- <pdf>Media:Draft_Sanchez Pinedo_983382402589_abstract.pdf</pdf> -->
 == Full Paper ==
 <pdf>Media:Draft_Sanchez Pinedo_983382402589_paper.pdf</pdf>

← Older revision		Revision as of 13:56, 22 November 2022
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	== Abstract ==		== Abstract ==
	<pdf>Media:Draft_Sanchez Pinedo_983382402589_abstract.pdf</pdf>		<pdf>Media:Draft_Sanchez Pinedo_983382402589_abstract.pdf</pdf>
		+
		+	== Full Paper ==
		+	<pdf>Media:Draft_Sanchez Pinedo_983382402589_paper.pdf</pdf>

← Older revision		Revision as of 13:56, 22 November 2022
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	In this work, a high-order implicit large-eddy simulation of an oblique shockwave/boundary layer interaction at Mach 2.3 is performed. The high-order solver is based on the flux reconstruction method, allowing an arbitrary order of accuracy. A particular attention is paid to the shock-capturing technique which consists in a combination of a Laplacian artificial viscosity with the Ducros sensor. The ability of such a solver to accurately predict the flow features is assessed on both steady and unsteady fields. In particular, the typical lowfrequency motion of the reflected shock is reproduced. The shock-capturing methodology is proven to be efficient at resolving the shocks without damping the turbulence in the boundary layer. The results obtained give confidence in this solver to study in more details the shockwave/boundary layer interaction phenomenon and future work is focused on the analysis of the oscillatory turbulent field in the interaction region.		In this work, a high-order implicit large-eddy simulation of an oblique shockwave/boundary layer interaction at Mach 2.3 is performed. The high-order solver is based on the flux reconstruction method, allowing an arbitrary order of accuracy. A particular attention is paid to the shock-capturing technique which consists in a combination of a Laplacian artificial viscosity with the Ducros sensor. The ability of such a solver to accurately predict the flow features is assessed on both steady and unsteady fields. In particular, the typical lowfrequency motion of the reflected shock is reproduced. The shock-capturing methodology is proven to be efficient at resolving the shocks without damping the turbulence in the boundary layer. The results obtained give confidence in this solver to study in more details the shockwave/boundary layer interaction phenomenon and future work is focused on the analysis of the oscillatory turbulent field in the interaction region.
		+
		+	== Abstract ==
		+	<pdf>Media:Draft_Sanchez Pinedo_983382402589_abstract.pdf</pdf>

← Older revision	Revision as of 13:56, 22 November 2022
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	+
	+	==Summary==

	+	In this work, a high-order implicit large-eddy simulation of an oblique shockwave/boundary layer interaction at Mach 2.3 is performed. The high-order solver is based on the flux reconstruction method, allowing an arbitrary order of accuracy. A particular attention is paid to the shock-capturing technique which consists in a combination of a Laplacian artificial viscosity with the Ducros sensor. The ability of such a solver to accurately predict the flow features is assessed on both steady and unsteady fields. In particular, the typical lowfrequency motion of the reflected shock is reproduced. The shock-capturing methodology is proven to be efficient at resolving the shocks without damping the turbulence in the boundary layer. The results obtained give confidence in this solver to study in more details the shockwave/boundary layer interaction phenomenon and future work is focused on the analysis of the oscillatory turbulent field in the interaction region.

← Older revision	Revision as of 15:06, 25 November 2022
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