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Toward an Efficient Icing CFD Process Using an Interactive Software Toolkit--SmaggIce 2DTwo-dimensional CFD analysis for iced airfoils can be a labor-intensive task. The software toolkit SmaggIce 2D is being developed to help streamline the CFD process and provide the unique features needed for icing. When complete, it will include a combination of partially automated and fully interactive tools for all aspects of the tasks leading up to the flow analysis: geometry preparation, domain decomposition, block boundary discretization. gridding, and linking with a flow solver. It also includes tools to perform ice shape characterization, an important aid in determining the relationship between ice characteristics and their effects on aerodynamic performance. Completed tools, work-in-progress, and planned features of the software toolkit are presented here.
Document ID
20030006685
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Vickerman, Mary B.
(NASA Glenn Research Center Cleveland, OH United States)
Choo, Yung K.
(NASA Glenn Research Center Cleveland, OH United States)
Schilling, Herbert W.
(NASA Glenn Research Center Cleveland, OH United States)
Baez, Marivell
(NASA Glenn Research Center Cleveland, OH United States)
Braun, Donald C.
(NASA Glenn Research Center Cleveland, OH United States)
Cotton, Barbara J.
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
August 21, 2013
Publication Date
December 1, 2002
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
NASA/TM-2001-211338
E-13149
AIAA Paper 2002-0380
NAS 1.15:211338
Meeting Information
Meeting: 40th AIAA Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 14, 2002
End Date: January 17, 2002
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
PROJECT: RTOP 711-20-23
Distribution Limits
Public
Copyright
Public Use Permitted.
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