| タイトル | Interactive Software System Developed to Study How Icing Affects Airfoil Performance (Phase 1 Results) |
| 本文（外部サイト） | http://hdl.handle.net/2060/20050192373 |
| 著者（英） | Vickerman, Mary B.; Choo, Yung K. |
| 著者所属（英） | NASA Glenn Research Center |
| 発行日 | 2000-03-01 |
| 言語 | eng |
| 内容記述 | SmaggIce (Surface Modeling and Grid Generation for Iced Airfoils), which is being developed at the NASA Glenn Research Center at Lewis Field, is an interactive software system for data probing, boundary smoothing, domain decomposition, and structured grid generation and refinement. All these steps are required for aerodynamic performance prediction using structured, grid-based computational fluid dynamics (CFD), as illustrated in the following figure. SmaggIce provides the underlying computations to perform these functions, as well as a graphical user interface to control and interact with them, and graphics to display the results. |
| NASA分類 | Computer Programming and Software |
| 権利 | No Copyright |
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