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Implementation of Combined Feather and Surface-Normal Ice Growth Models in LEWICE/XExperimental observations have shown that discrete rime ice growths called feathers, which grow in approximately the direction of water droplet impingement, play an important role in the growth of ice on accreting surfaces for some thermodynamic conditions. An improved physical model of ice accretion has been implemented in the LEWICE 2D panel-based ice accretion code maintained by the NASA Lewis Research Center. The LEWICE/X model of ice accretion explicitly simulates regions of feather growth within the framework of the LEWICE model. Water droplets impinging on an accreting surface are withheld from the normal LEWICE mass/energy balance and handled in a separate routine; ice growth resulting from these droplets is performed with enhanced convective heat transfer approximately along droplet impingement directions. An independent underlying ice shape is grown along surface normals using the unmodified LEWICE method. The resulting dual-surface ice shape models roughness-induced feather growth observed in icing wind tunnel tests. Experiments indicate that the exact direction of feather growth is dependent on external conditions. Data is presented to support a linear variation of growth direction with temperature and cloud water content. Test runs of LEWICE/X indicate that the sizes of surface regions containing feathers are influenced by initial roughness element height. This suggests that a previous argument that feather region size is determined by boundary layer transition may be incorrect. Simulation results for two typical test cases give improved shape agreement over unmodified LEWICE.
Document ID
19970040868
Acquisition Source
Headquarters
Document Type
Reprint (Version printed in journal)
Authors
Velazquez, M. T.
(Massachusetts Inst. of Tech. Cambridge, MA United States)
Hansman, R. J., Jr.
(Massachusetts Inst. of Tech. Cambridge, MA United States)
Date Acquired
August 17, 2013
Publication Date
January 1, 1995
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA/CR-95-112615
AIAA Paper 95-0753
NAS 1.26:112615
Meeting Information
Meeting: Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 9, 1995
End Date: January 12, 1995
Sponsors: American Inst. of Aeronautics and Astronautics
Accession Number
97N72527
Funding Number(s)
CONTRACT_GRANT: NGL-22-0069-640
CONTRACT_GRANT: NAGw-1761
Distribution Limits
Public
Copyright
Public Use Permitted.
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