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Advancements in the LEWICE Ice Accretion ModelRecent evidence has shown that the NASA/Lewis Ice Accretion Model, LEWICE, does not predict accurate ice shapes for certain glaze ice conditions. This paper will present the methodology used to make a first attempt at improving the ice accretion prediction in these regimes. Importance is given to the correlations for heat transfer coefficient and ice density, as well as runback flow, selection of the transition point, flow field resolution, and droplet trajectory models. Further improvements and refinement of these modules will be performed once tests in NASA's Icing Research Tunnel, scheduled for 1993, are completed.
Document ID
19930006213
Acquisition Source
Glenn Research Center
Document Type
Contractor Report (CR)
Authors
William B Wright
(Sverdrup Maryland Heights, Missouri, United States)
Date Acquired
September 6, 2013
Publication Date
January 11, 1993
Publication Information
Publication: 31st Aerospace Sciences Meeting
Publisher: American Institute of Aeronautics and Astronautics
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
AIAA PAPER 93-0171
NAS 1.26:191019
E-7523
NASA-CR-191019
Report Number: AIAA PAPER 93-0171
Report Number: NAS 1.26:191019
Report Number: E-7523
Report Number: NASA-CR-191019
Meeting Information
Meeting: 31st Aerospace Sciences Meeting
Location: Reno, NV
Country: US
Start Date: January 11, 1993
End Date: January 14, 1993
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
93N15402
Funding Number(s)
CONTRACT_GRANT: NAS3-25266
PROJECT: RTOP 505-68-10
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Icing
Computational methods
Icing conditions
Heat transfer coefficients
Stagnation point
Two dimensional flow
Thermal diffusivity
Kinematic viscosity
Boundary layer thickness
Angle of attack
Thermal properties
Thermal conductivity
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