Internal:Adaptive CDT3D Results - Revision history

Ctsolakis at 20:49, 17 February 2020

2020-02-17T20:49:44Z

← Older revision		Revision as of 16:49, 17 February 2020
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	Description (<ref>M. A. Park et al., “Unstructured Grid Adaptation and Solver Technology for Turbulent Flows,” in 2018 AIAA Aerospace Sciences Meeting,https://arc.aiaa.org/doi/abs/10.2514/6.2018-1103</ref> )		Description (<ref>M. A. Park et al., “Unstructured Grid Adaptation and Solver Technology for Turbulent Flows,” in 2018 AIAA Aerospace Sciences Meeting,https://arc.aiaa.org/doi/abs/10.2514/6.2018-1103</ref> )
	This case comes from the LaRC Turbulent Modeling Resource. For more see https://turbmodels.larc.nasa.gov/onerawingnumerics_val.html		This case comes from the LaRC Turbulent Modeling Resource. For more see https://turbmodels.larc.nasa.gov/onerawingnumerics_val.html

			{{Reflist}}

	[[Internal:CDT3D_OneraM6_adaptation_2020]]		[[Internal:CDT3D_OneraM6_adaptation_2020]]
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	'''Description (<ref>M. A. Park et al., “Unstructured Grid Adaptation and Solver Technology for Turbulent Flows,” in 2018 AIAA Aerospace Sciences Meeting,https://arc.aiaa.org/doi/abs/10.2514/6.2018-1103</ref> ) ''' This case comes from the LaRC Turbulent Modeling Resource. For more see https://turbmodels.larc.nasa.gov/hc3dnumericspart2_val.html		'''Description (<ref>M. A. Park et al., “Unstructured Grid Adaptation and Solver Technology for Turbulent Flows,” in 2018 AIAA Aerospace Sciences Meeting,https://arc.aiaa.org/doi/abs/10.2514/6.2018-1103</ref> ) ''' This case comes from the LaRC Turbulent Modeling Resource. For more see https://turbmodels.larc.nasa.gov/hc3dnumericspart2_val.html

			{{Reflist}}

	[[Internal:CDT3D_Hemicyl_2020]]		[[Internal:CDT3D_Hemicyl_2020]]

Ctsolakis at 23:35, 10 February 2020

2020-02-10T23:35:02Z

← Older revision		Revision as of 19:35, 10 February 2020
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	Description (<ref>M. A. Park et al., “Unstructured Grid Adaptation and Solver Technology for Turbulent Flows,” in 2018 AIAA Aerospace Sciences Meeting,https://arc.aiaa.org/doi/abs/10.2514/6.2018-1103</ref> )		Description (<ref>M. A. Park et al., “Unstructured Grid Adaptation and Solver Technology for Turbulent Flows,” in 2018 AIAA Aerospace Sciences Meeting,https://arc.aiaa.org/doi/abs/10.2514/6.2018-1103</ref> )
	This case comes from the LaRC Turbulent Modeling Resource. For more see https://turbmodels.larc.nasa.gov/onerawingnumerics_val.html		This case comes from the LaRC Turbulent Modeling Resource. For more see https://turbmodels.larc.nasa.gov/onerawingnumerics_val.html

			[[Internal:CDT3D_OneraM6_adaptation_2020]]

	= Hemisphere Cylinder =		= Hemisphere Cylinder =

Ctsolakis: /* OneraM6 Wing */

2020-02-10T23:34:19Z

OneraM6 Wing

← Older revision		Revision as of 19:34, 10 February 2020
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	[[File:Onera m6.png\|500px]]		[[File:Onera m6.png\|500px]]

	Description (<ref>M. A. Park et al., “Unstructured Grid Adaptation and Solver Technology for Turbulent Flows,” in 2018 AIAA Aerospace Sciences Meeting,https://arc.aiaa.org/doi/abs/10.2514/6.2018-1103</ref> ) ~~'''~~ This case comes from the LaRC Turbulent Modeling Resource. For more see		Description (<ref>M. A. Park et al., “Unstructured Grid Adaptation and Solver Technology for Turbulent Flows,” in 2018 AIAA Aerospace Sciences Meeting,https://arc.aiaa.org/doi/abs/10.2514/6.2018-1103</ref> )
			This case comes from the LaRC Turbulent Modeling Resource. For more see https://turbmodels.larc.nasa.gov/onerawingnumerics_val.html

	~~https://turbmodels.larc.nasa.gov/onerawingnumerics_val.html~~
	= Hemisphere Cylinder =		= Hemisphere Cylinder =
	[[ File:Hemicyl.png ‎ \|500px]]		[[ File:Hemicyl.png ‎ \|500px]]

Ctsolakis at 23:33, 10 February 2020

2020-02-10T23:33:40Z

← Older revision		Revision as of 19:33, 10 February 2020
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			=OneraM6 Wing =
			[[File:Onera m6.png\|500px]]

			Description (<ref>M. A. Park et al., “Unstructured Grid Adaptation and Solver Technology for Turbulent Flows,” in 2018 AIAA Aerospace Sciences Meeting,https://arc.aiaa.org/doi/abs/10.2514/6.2018-1103</ref> ) ''' This case comes from the LaRC Turbulent Modeling Resource. For more see

			https://turbmodels.larc.nasa.gov/onerawingnumerics_val.html
	= Hemisphere Cylinder =		= Hemisphere Cylinder =
	[[ File:Hemicyl.png ‎ \|500px]]		[[ File:Hemicyl.png ‎ \|500px]]

Ctsolakis: /* Hemisphere Cylinder */

2020-02-10T22:36:00Z

Hemisphere Cylinder

← Older revision		Revision as of 18:36, 10 February 2020
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	[[ File:Hemicyl.png ‎ \|500px]]		[[ File:Hemicyl.png ‎ \|500px]]

	'''Description (<ref>M. A. Park et al., “Unstructured Grid Adaptation and Solver Technology for Turbulent Flows,” in 2018 AIAA Aerospace Sciences Meeting,https://arc.aiaa.org/doi/abs/10.2514/6.2018-1103</ref> ) '''		'''Description (<ref>M. A. Park et al., “Unstructured Grid Adaptation and Solver Technology for Turbulent Flows,” in 2018 AIAA Aerospace Sciences Meeting,https://arc.aiaa.org/doi/abs/10.2514/6.2018-1103</ref> ) ''' This case comes from the LaRC Turbulent Modeling Resource. For more see https://turbmodels.larc.nasa.gov/hc3dnumericspart2_val.html

	[[Internal:CDT3D_Hemicyl_2020]]		[[Internal:CDT3D_Hemicyl_2020]]

Ctsolakis: /* Hemisphere Cylinder */

2020-02-10T22:30:35Z

Hemisphere Cylinder

← Older revision		Revision as of 18:30, 10 February 2020
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	[[ File:Hemicyl.png ‎ \|500px]]		[[ File:Hemicyl.png ‎ \|500px]]

	'''Description (<ref> ~~[1][1]~~M. A. Park et al., “Unstructured Grid Adaptation and Solver Technology for Turbulent Flows,” in 2018 AIAA Aerospace Sciences Meeting,https://arc.aiaa.org/doi/abs/10.2514/6.2018-1103</ref> ) '''		'''Description (<ref>M. A. Park et al., “Unstructured Grid Adaptation and Solver Technology for Turbulent Flows,” in 2018 AIAA Aerospace Sciences Meeting,https://arc.aiaa.org/doi/abs/10.2514/6.2018-1103</ref> ) '''

			[[Internal:CDT3D_Hemicyl_2020]]

	= Delta Wing =		= Delta Wing =

Ctsolakis at 22:28, 10 February 2020

2020-02-10T22:28:57Z

← Older revision		Revision as of 18:28, 10 February 2020
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	= Hemisphere Cylinder =		= Hemisphere Cylinder =
	[[ File:Hemicyl.png ‎ \|500px]]		[[ File:Hemicyl.png ‎ \|500px]]

			'''Description (<ref> [1][1]M. A. Park et al., “Unstructured Grid Adaptation and Solver Technology for Turbulent Flows,” in 2018 AIAA Aerospace Sciences Meeting,https://arc.aiaa.org/doi/abs/10.2514/6.2018-1103</ref> ) '''
	= Delta Wing =		= Delta Wing =

Ctsolakis at 22:24, 10 February 2020

2020-02-10T22:24:20Z

← Older revision		Revision as of 18:24, 10 February 2020
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			= Hemisphere Cylinder =
			[[ File:Hemicyl.png ‎ \|500px]]
	= Delta Wing =		= Delta Wing =

Ctsolakis: /* Cube (polar-2 metric) */

2019-09-04T18:41:35Z

Cube (polar-2 metric)

← Older revision		Revision as of 14:41, 4 September 2019
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	'''Description (scitech 2018): ''' A cube with an analytically defined metric field M referred to as polar-2 in the first UGAWG benchmark [https://www.sciencedirect.com/science/article/pii/S1877705817343618].		'''Description (scitech 2018): ''' A cube with an analytically defined metric field M referred to as polar-2 in the first UGAWG benchmark [https://www.sciencedirect.com/science/article/pii/S1877705817343618].

			[[Internal:CDT3D_Strong_Scaling_cube_case\| Strong Scaling Data (2019)]]


	[[Internal:ACDT3D_(Scitech2018)_Strong_Scaling_(Cube_case)\| Strong Scaling Data (Scitech 2018)]]		[[Internal:ACDT3D_(Scitech2018)_Strong_Scaling_(Cube_case)\| Strong Scaling Data (Scitech 2018)]]

Ctsolakis: /* Cube (polar-2 metric) */

2019-09-04T18:40:13Z

Cube (polar-2 metric)

← Older revision		Revision as of 14:40, 4 September 2019
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	[[File:Cube_qcircle1.png\|300px]]		[[File:Cube_qcircle1.png\|300px]]

	'''Description (scitech 2018): ''' A cube with an analytically defined metric field M referred to as polar-2 in the first UGAWG benchmark.		'''Description (scitech 2018): ''' A cube with an analytically defined metric field M referred to as polar-2 in the first UGAWG benchmark [https://www.sciencedirect.com/science/article/pii/S1877705817343618].

	[[Internal:ACDT3D_(Scitech2018)_Strong_Scaling_(Cube_case)\| Strong Scaling Data (Scitech 2018)]]		[[Internal:ACDT3D_(Scitech2018)_Strong_Scaling_(Cube_case)\| Strong Scaling Data (Scitech 2018)]]