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collection efficiency and ice accretion characteristics of two full scale and one 1/4 scale business jet horizontal tailsCollection efficiency and ice accretion calculations have been made for a series of business jet horizontal tail configurations using a three-dimensional panel code, an adaptive grid code, and the NASA Glenn LEWICE3D grid based ice accretion code. The horizontal tail models included two full scale wing tips and a 25 percent scale model. Flow solutions for the horizontal tails were generated using the PMARC panel code. Grids used in the ice accretion calculations were generated using the adaptive grid code ICEGRID. The LEWICE3D grid based ice accretion program was used to calculate impingement efficiency and ice shapes. Ice shapes typifying rime and mixed icing conditions were generated for a 30 minute hold condition. All calculations were performed on an SGI Octane computer. The results have been compared to experimental flow and impingement data. In general, the calculated flow and collection efficiencies compared well with experiment, and the ice shapes appeared representative of the rime and mixed icing conditions for which they were calculated.
Document ID
20050186904
Document Type
Technical Memorandum (TM)
Authors
Bidwell, Colin S.
(NASA Glenn Research Center Cleveland, OH, United States)
Papadakis, Michael
(Wichita State Univ. Wichita, KS, United States)
Date Acquired
September 7, 2013
Publication Date
June 1, 2005
Subject Category
Fluid Mechanics and Thermodynamics
Report/Patent Number
E-15142
SAE-2000-01-1683
NASA/TM-2005-213653
Meeting Information
SAE General Aviation Technology Conference and Exposition(Wichita, KS)
Funding Number(s)
WBS: WBS 22-077-41-08
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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