Modelling programs: Difference between revisions

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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.  






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Revision as of 11:37, 10 February 2022

[1]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.

Modern CFD tools such as LEWICE [2] [3] [4] and FENSAP-ICE [5] [6] 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.


[1]

  1. 1.0 1.1 Ansys FENSAP-ICE: Ice Accretion Simulation Software, Ansys, webpage, available (accessed 4.3.2021): https://www.ansys.com/products/fluids/ansysfensap-ice/fensap-ice-capabilities
  2. William B. Wright, User manual for the NASA Glenn Ice Accretion code LEWICE version 2.2.2, NASA/CR 2002-211793, NASA, 2002.
  3. William B. Wright, Validation results for LEWICE 3.0, NASA-2005-1243, NASA, 2005.
  4. 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.
  5. ANSYS FENSAP-ICE user manual, ANSYS, 2016.
  6. 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.