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Users Manual for the NASA Lewis Ice Accretion Prediction Code (LEWICE)LEWICE is an ice accretion prediction code that applies a time-stepping procedure to calculate the shape of an ice accretion. The potential flow field is calculated in LEWICE using the Douglas Hess-Smith 2-D panel code (S24Y). This potential flow field is then used to calculate the trajectories of particles and the impingement points on the body. These calculations are performed to determine the distribution of liquid water impinging on the body, which then serves as input to the icing thermodynamic code. The icing thermodynamic model is based on the work of Messinger, but contains several major modifications and improvements. This model is used to calculate the ice growth rate at each point on the surface of the geometry. By specifying an icing time increment, the ice growth rate can be interpreted as an ice thickness which is added to the body, resulting in the generation of new coordinates. This procedure is repeated, beginning with the potential flow calculations, until the desired icing time is reached. The operation of LEWICE is illustrated through the use of five examples. These examples are representative of the types of applications expected for LEWICE. All input and output is discussed, along with many of the diagnostic messages contained in the code. Several error conditions that may occur in the code for certain icing conditions are identified, and a course of action is recommended. LEWICE has been used to calculate a variety of ice shapes, but should still be considered a research code. The code should be exercised further to identify any shortcomings and inadequacies. Any modifications identified as a result of these cases, or of additional experimental results, should be incorporated into the model. Using it as a test bed for improvements to the ice accretion model is one important application of LEWICE.
Document ID
19900011627
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Ruff, Gary A.
(Sverdrup Technology, Inc. Brook Park, OH, United States)
Berkowitz, Brian M.
(Sverdrup Technology, Inc. Brook Park, OH, United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1990
Subject Category
Aeronautics (General)
Report/Patent Number
NAS 1.26:185129
NASA-CR-185129
GRC-E-DAA-TN10592
Accession Number
90N20943
Funding Number(s)
CONTRACT_GRANT: NAS3-25266
PROJECT: RTOP 505-68-11
Distribution Limits
Public
Copyright
Public Use Permitted.
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