タイトル | SmaggIce Version 1.8 |
本文(外部サイト) | http://hdl.handle.net/2060/20110013103 |
著者(英) | Braun, Donald C.; Wilson, Barbara J.; Schilling, Herbert W.; Hackenberg, Anthony W.; Pennline, James A.; Coroneos, Rula M.; Vickerman, Mary B.; Baez, Marivell; Choo, Yung K. |
著者所属(英) | NASA Glenn Research Center |
発行日 | 2006-09-01 |
言語 | eng |
内容記述 | SmaggIce version 1.8 is a set of software tools for geometrical modeling of, and generation of grids that conform to, both clean and iced airfoils. Ice shapes, especially those that include rough surfaces, pose difficulty in generating high-quality grids that are essential for predicting airflows by use of computational fluid dynamics. SmaggIce version 1.8 contains software tools needed to overcome this difficulty. For a given airfoil, it allows the user to define the flow domain, decompose the domain into blocks, generate grids, merge gridded blocks, and control the density and smoothness of each grid. Among the unique features of version 1.8 is a thin C-shaped block, called a "viscous sublayer block," which is wrapped around an iced airfoil and its wake line and serves as a means to generate highly controlled grids near the rough ice surface. Users can modify block boundary shapes using control points of non-uniform rational B-spline (NURBS) curves. Concave ice regions can be smoothed during geometrical modeling or creation of the viscous sublayer block. |
NASA分類 | Man/System Technology and Life Support |
レポートNO | LEW-17846-1 |
権利 | Copyright, Distribution as joint owner in the copyright |
URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/499399 |
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