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A Summary of Validation Results for LEWICE 2.0A research project is underway at NASA Lewis to produce a computer code which can accurately predict ice growth under any meteorological conditions for any aircraft surface. This report will present results from version 2.0 of this code, which is called LEWICE. This version differs from previous releases due to its robustness and its ability to reproduce results accurately for different point spacing, and time step criteria across general computing platforms. It also differs in the extensive amount of effort undertaken to compare the results in a quantifiable manner against the database of ice shapes which have been generated in the NASA Lewis Icing, Research Tunnel (IRT), The complete set of data used for this comparison is available in a recent contractor report . The result of this comparison shows that the difference between the predicted ice shape from LEWICE 2.0 and the average of the experimental data is 7.2% while the variability of the experimental data is 2.5%.
Document ID
19990017993
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Wright, William B.
(DYNACS Engineering Co., Inc. Brook Park, OH United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1998
Subject Category
Aerodynamics
Report/Patent Number
E-11467
NASA/CR-1998-208687
AIAA Paper 99-0249
NAS 1.26:208687
Meeting Information
Meeting: Aerospace Sciences
Location: Reno, NV
Country: United States
Start Date: January 11, 1999
End Date: January 14, 1999
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
PROJECT: RTOP 548-20-23
CONTRACT_GRANT: NAS3-98022
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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