Super Cooled Large Droplet Analysis for Several Geometries Using LEWICE3D Version 3 | Zendy

Colin S. Bidwell | Zendy

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Super Cooled Large Droplet Analysis for Several Geometries Using LEWICE3D Version 3

Author(s) -

Colin S. Bidwell

Publication year - 2010

Publication title -

nasa sti repository (national aeronautics and space administration)

Language(s) - English

Resource type - Conference proceedings

DOI - 10.2514/6.2010-7675

Subject(s) - computation , software , lift (data mining) , wing , computer science , aerospace engineering , computer graphics (images) , computational science , engineering , algorithm , operating system , data mining

Super Cooled Large Droplet (SLD) collection efficiency calculations were performed for several geometries using the LEWICE3D Version 3 software. The computations were performed using the NASA Glenn Research Center SLD splashing model which has been incorporated into the LEWICE3D Version 3 software. Comparisons to experiment were made where available. The geometries included two straight wings, a swept 64A008 wing tip, two high lift geometries, and the generic commercial transport DLR-F4 wing body configuration. In general the LEWICE3D Version 3 computations compared well with the 2D LEWICE 3.2.2 results and with experimental data where available.

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