Modelling programs - Revision history

Novia at 08:53, 11 February 2022

2022-02-11T08:53:46Z

← Older revision		Revision as of 11:53, 11 February 2022
Line 5:		Line 5:

	FLUENT is a CFD- code for modelling fluid flow, heat transfer, mass transfer and chemical reactions. <ref>swMATH. Online. https://swmath.org/software/4263</ref>		FLUENT is a CFD- code for modelling fluid flow, heat transfer, mass transfer and chemical reactions. <ref>swMATH. Online. https://swmath.org/software/4263</ref>




	<ref name=":0" />		<ref name=":0" />

			== References ==
			<references />

Novia at 08:46, 10 February 2022

2022-02-10T08:46:05Z

← Older revision		Revision as of 11:46, 10 February 2022
Line 2:		Line 2:
	Icing modelling programs can be used for simulating icing. Icing modelling programs are used for example in calculating shape and size of accreted ice. Modelling programs are commonly used for modelling icing on aircrafts.		Icing modelling programs can be used for simulating icing. Icing modelling programs are used for example in calculating shape and size of accreted ice. Modelling programs are commonly used for modelling icing on aircrafts.

	Modern [[CFD]] tools such as LEWICE <ref>William B. Wright, User manual for the NASA Glenn Ice Accretion code LEWICE version 2.2.2, NASA/CR 2002-211793, NASA, 2002.</ref> <ref>William B. Wright, Validation results for LEWICE 3.0, NASA-2005-1243, NASA, 2005.</ref> <ref>Colin S. Bidwell and Mark G. Potapczuk, Users manual for the NASA Lewis three-dimensional ice accretion code (LEWICE3D), NASA Technical Memorandum 105974, NASA, 1993.</ref> and FENSAP-ICE <ref>ANSYS FENSAP-ICE user manual, ANSYS, 2016.</ref> <ref>Héloïse Beaugendre, François Morency, and Wagdi G. Habashi, FENSAP-ICE's threedimensional in-flight ice accretion module : ICE3D, Jounal of Aircraft, vol. 40, no. 2, pp. 239 – 247, 2003.</ref> are capable of modelling the icing in both the 2D and the 3D cases, as their main objective is the estimation of the geometry change due to icing.		Modern [[CFD]] tools such as LEWICE <ref>William B. Wright, User manual for the NASA Glenn Ice Accretion code LEWICE version 2.2.2, NASA/CR 2002-211793, NASA, 2002.</ref> <ref>William B. Wright, Validation results for LEWICE 3.0, NASA-2005-1243, NASA, 2005.</ref> <ref>Colin S. Bidwell and Mark G. Potapczuk, Users manual for the NASA Lewis three-dimensional ice accretion code (LEWICE3D), NASA Technical Memorandum 105974, NASA, 1993.</ref> and FENSAP-ICE <ref>ANSYS FENSAP-ICE user manual, ANSYS, 2016.</ref> <ref>Héloïse Beaugendre, François Morency, and Wagdi G. Habashi, FENSAP-ICE's threedimensional in-flight ice accretion module : ICE3D, Jounal of Aircraft, vol. 40, no. 2, pp. 239 – 247, 2003.</ref> are capable of modelling the icing in both the 2D and the 3D cases, as their main objective is the estimation of the geometry change due to icing. <ref>Jia Yi Jin. Study of Atmospheric Ice Accretion on Wind Turbine Blades. 2021. Thesis for the degree of Philosophiae Doctor. UiT ̶ The Arctic University of Norway Faculty of Engineering Science and Technology.</ref>

	FLUENT is a CFD- code for modelling fluid flow, heat transfer, mass transfer and chemical reactions. <ref>swMATH. Online. https://swmath.org/software/4263</ref>		FLUENT is a CFD- code for modelling fluid flow, heat transfer, mass transfer and chemical reactions. <ref>swMATH. Online. https://swmath.org/software/4263</ref>

Novia at 08:45, 10 February 2022

2022-02-10T08:45:05Z

← Older revision		Revision as of 11:45, 10 February 2022
Line 2:		Line 2:
	Icing modelling programs can be used for simulating icing. Icing modelling programs are used for example in calculating shape and size of accreted ice. Modelling programs are commonly used for modelling icing on aircrafts.		Icing modelling programs can be used for simulating icing. Icing modelling programs are used for example in calculating shape and size of accreted ice. Modelling programs are commonly used for modelling icing on aircrafts.

	Modern [[CFD]] tools such as LEWICE <ref>William B. Wright, User manual for the NASA Glenn Ice Accretion code LEWICE version 2.2.2, NASA/CR 2002-211793, NASA, 2002.</ref> <ref>William B. Wright, Validation results for LEWICE 3.0, NASA-2005-1243, NASA, 2005.</ref> <ref>Colin S. Bidwell and Mark G. Potapczuk, Users manual for the NASA Lewis three-dimensional ice accretion code (LEWICE3D), NASA Technical Memorandum 105974, NASA, 1993.</ref> and FENSAP-ICE <ref>ANSYS FENSAP-ICE user manual, ANSYS, 2016.</ref> <ref>Héloïse Beaugendre, François Morency, and Wagdi G. Habashi, FENSAP-ICE's threedimensional in-flight ice accretion module : ICE3D, Jounal of Aircraft, vol. 40, no. 2, pp. 239 – 247, 2003.</ref> are capable of modelling the icing in both the 2D and the 3D cases, as their main objective is the estimation of the geometry change due to icing.		Modern [[CFD]] tools such as LEWICE <ref>William B. Wright, User manual for the NASA Glenn Ice Accretion code LEWICE version 2.2.2, NASA/CR 2002-211793, NASA, 2002.</ref> <ref>William B. Wright, Validation results for LEWICE 3.0, NASA-2005-1243, NASA, 2005.</ref> <ref>Colin S. Bidwell and Mark G. Potapczuk, Users manual for the NASA Lewis three-dimensional ice accretion code (LEWICE3D), NASA Technical Memorandum 105974, NASA, 1993.</ref> and FENSAP-ICE <ref>ANSYS FENSAP-ICE user manual, ANSYS, 2016.</ref> <ref>Héloïse Beaugendre, François Morency, and Wagdi G. Habashi, FENSAP-ICE's threedimensional in-flight ice accretion module : ICE3D, Jounal of Aircraft, vol. 40, no. 2, pp. 239 – 247, 2003.</ref> are capable of modelling the icing in both the 2D and the 3D cases, as their main objective is the estimation of the geometry change due to icing.

			FLUENT is a CFD- code for modelling fluid flow, heat transfer, mass transfer and chemical reactions. <ref>swMATH. Online. https://swmath.org/software/4263</ref>




	<ref name=":0" />		<ref name=":0" />

Novia at 08:37, 10 February 2022

2022-02-10T08:37:22Z

← Older revision		Revision as of 11:37, 10 February 2022
Line 2:		Line 2:
	Icing modelling programs can be used for simulating icing. Icing modelling programs are used for example in calculating shape and size of accreted ice. Modelling programs are commonly used for modelling icing on aircrafts.		Icing modelling programs can be used for simulating icing. Icing modelling programs are used for example in calculating shape and size of accreted ice. Modelling programs are commonly used for modelling icing on aircrafts.

	Modern CFD tools such as LEWICE <ref>William B. Wright, User manual for the NASA Glenn Ice Accretion code LEWICE version 2.2.2, NASA/CR 2002-211793, NASA, 2002.</ref> <ref>William B. Wright, Validation results for LEWICE 3.0, NASA-2005-1243, NASA, 2005.</ref> <ref>Colin S. Bidwell and Mark G. Potapczuk, Users manual for the NASA Lewis three-dimensional ice accretion code (LEWICE3D), NASA Technical Memorandum 105974, NASA, 1993.</ref> and FENSAP-ICE <ref>ANSYS FENSAP-ICE user manual, ANSYS, 2016.</ref> <ref>Héloïse Beaugendre, François Morency, and Wagdi G. Habashi, FENSAP-ICE's threedimensional in-flight ice accretion module : ICE3D, Jounal of Aircraft, vol. 40, no. 2, pp. 239 – 247, 2003.</ref> are capable of modelling the icing in both the 2D and the 3D cases, as their main objective is the estimation of the geometry change due to icing.		Modern [[CFD]] tools such as LEWICE <ref>William B. Wright, User manual for the NASA Glenn Ice Accretion code LEWICE version 2.2.2, NASA/CR 2002-211793, NASA, 2002.</ref> <ref>William B. Wright, Validation results for LEWICE 3.0, NASA-2005-1243, NASA, 2005.</ref> <ref>Colin S. Bidwell and Mark G. Potapczuk, Users manual for the NASA Lewis three-dimensional ice accretion code (LEWICE3D), NASA Technical Memorandum 105974, NASA, 1993.</ref> and FENSAP-ICE <ref>ANSYS FENSAP-ICE user manual, ANSYS, 2016.</ref> <ref>Héloïse Beaugendre, François Morency, and Wagdi G. Habashi, FENSAP-ICE's threedimensional in-flight ice accretion module : ICE3D, Jounal of Aircraft, vol. 40, no. 2, pp. 239 – 247, 2003.</ref> are capable of modelling the icing in both the 2D and the 3D cases, as their main objective is the estimation of the geometry change due to icing.



	<ref name=":0" />		<ref name=":0" />

Novia at 08:35, 10 February 2022

2022-02-10T08:35:52Z

← Older revision		Revision as of 11:35, 10 February 2022
Line 1:		Line 1:
	[[File:Fensap.jpg\|thumb\|595x595px\|<ref name=":0">Ansys FENSAP-ICE: Ice Accretion Simulation Software, Ansys, webpage, available (accessed 4.3.2021): <nowiki>https://www.ansys.com/products/fluids/ansysfensap-ice/fensap-ice-capabilities</nowiki></ref>Simulated ice accretion on an airplane wing created using FENSAP-ICE.]]		[[File:Fensap.jpg\|thumb\|595x595px\|<ref name=":0">Ansys FENSAP-ICE: Ice Accretion Simulation Software, Ansys, webpage, available (accessed 4.3.2021): <nowiki>https://www.ansys.com/products/fluids/ansysfensap-ice/fensap-ice-capabilities</nowiki></ref>Simulated ice accretion on an airplane wing created using FENSAP-ICE.]]
	Icing modelling programs can be used for simulating icing. Icing modelling programs are used for example in calculating shape and size of accreted ice. Modelling programs are commonly used for modelling icing on aircrafts.		Icing modelling programs can be used for simulating icing. Icing modelling programs are used for example in calculating shape and size of accreted ice. Modelling programs are commonly used for modelling icing on aircrafts.

			Modern CFD tools such as LEWICE <ref>William B. Wright, User manual for the NASA Glenn Ice Accretion code LEWICE version 2.2.2, NASA/CR 2002-211793, NASA, 2002.</ref> <ref>William B. Wright, Validation results for LEWICE 3.0, NASA-2005-1243, NASA, 2005.</ref> <ref>Colin S. Bidwell and Mark G. Potapczuk, Users manual for the NASA Lewis three-dimensional ice accretion code (LEWICE3D), NASA Technical Memorandum 105974, NASA, 1993.</ref> and FENSAP-ICE <ref>ANSYS FENSAP-ICE user manual, ANSYS, 2016.</ref> <ref>Héloïse Beaugendre, François Morency, and Wagdi G. Habashi, FENSAP-ICE's threedimensional in-flight ice accretion module : ICE3D, Jounal of Aircraft, vol. 40, no. 2, pp. 239 – 247, 2003.</ref> are capable of modelling the icing in both the 2D and the 3D cases, as their main objective is the estimation of the geometry change due to icing.



	<ref name=":0" />		<ref name=":0" />

Novia at 09:33, 22 December 2021

2021-12-22T09:33:53Z

← Older revision		Revision as of 12:33, 22 December 2021
Line 1:		Line 1:
			[[File:Fensap.jpg\|thumb\|595x595px\|<ref name=":0">Ansys FENSAP-ICE: Ice Accretion Simulation Software, Ansys, webpage, available (accessed 4.3.2021): <nowiki>https://www.ansys.com/products/fluids/ansysfensap-ice/fensap-ice-capabilities</nowiki></ref>Simulated ice accretion on an airplane wing created using FENSAP-ICE.]]
	Icing modelling programs can be used for simulating icing. Icing modelling programs are used for example in calculating shape and size of accreted ice. Modelling programs are commonly used for modelling icing on aircrafts.		Icing modelling programs can be used for simulating icing. Icing modelling programs are used for example in calculating shape and size of accreted ice. Modelling programs are commonly used for modelling icing on aircrafts.


			<ref name=":0" />

Novia: Created page with "Icing modelling programs can be used for simulating icing. Icing modelling programs are used for example in calculating shape and size of accreted ice. Modelling programs are..."

2021-12-22T09:31:21Z

Created page with "Icing modelling programs can be used for simulating icing. Icing modelling programs are used for example in calculating shape and size of accreted ice. Modelling programs are..."

New page

Icing modelling programs can be used for simulating icing. Icing modelling programs are used for example in calculating shape and size of accreted ice. Modelling programs are commonly used for modelling icing on aircrafts.