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SmaggIce 2.0: Additional Capabilities for Interactive Grid Generation of Iced AirfoilsThe Surface Modeling and Grid Generation for Iced Airfoils (SmaggIce) software toolkit has been extended to allow interactive grid generation for multi-element iced airfoils. The essential phases of an icing effects study include geometry preparation, block creation and grid generation. SmaggIce Version 2.0 now includes these main capabilities for both single and multi-element airfoils, plus an improved flow solver interface and a variety of additional tools to enhance the efficiency and accuracy of icing effects studies. An overview of these features is given, especially the new multi-element blocking strategy using the multiple wakes method. Examples are given which illustrate the capabilities of SmaggIce for conducting an icing effects study for both single and multi-element airfoils.
Document ID
20080010685
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Kreeger, Richard E.
(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)
Schilling, Herbert W.
(NASA Glenn Research Center Cleveland, OH, United States)
Vickerman, Mary B.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 24, 2013
Publication Date
January 1, 2008
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA/TM-2008-214829
AIAA Paper 2007-0502
E-16022
Report Number: NASA/TM-2008-214829
Report Number: AIAA Paper 2007-0502
Report Number: E-16022
Meeting Information
Meeting: 45th Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 8, 2007
End Date: January 11, 2007
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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