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Effect of Time-Step Duration and Other Parameters on Ice AccretionThis work addresses the ice prediction cases studies for the 1st AIAA Ice Prediction Workshop generated using a mix of commercial and in-house tools. All predictions are compared with those by LEWICE. Results from both 2D NACA 23012 airfoil cases and 3D NACA 0012 swept wing cases have been included. It is observed that the computational tools have a much better correlation with experimental data for rime icing conditions. For glaze icing conditions, the ice horns are not accurately predicted. The impact of parameters such as surface temperature, heat transfer coefficient, and time-step for flow and droplet field re-computation is explored.
Document ID
20220006403
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Avani Gupta
(Georgia Institute of Technology Atlanta, Georgia, United States)
Lakshmi N. Sankar
(Georgia Institute of Technology Atlanta, Georgia, United States)
Richard E Kreeger
(Glenn Research Center Cleveland, Ohio, United States)
Date Acquired
April 26, 2022
Subject Category
Aerodynamics
Meeting Information
Meeting: AIAA Aviation 2022
Location: Chicago IL
Country: US
Start Date: June 27, 2022
End Date: July 1, 2022
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 664817.02.03.03.03
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Technical Review
Single Expert
Keywords
Icing, Rotorcraft
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