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The Influence of SLD Drop Size Distributions on Ice Accretion in the NASA Icing Research TunnelAn ice shape database has been created to document ice accretions on a 21-inch chord NACA0012 model and a 72-inch chord NACA 23012 airfoil model resulting from an exposure to a Supercooled Large Drop (SLD) icing cloud with a bimodal drop size distribution. The ice shapes created were documented with photographs, laser scanned surface measurements over a section of the model span, and measurement of the ice mass over the same section of each accretion. The icing conditions used in the test matrix were based upon previously used conditions on the same models but with an alternate approach to evaluation of drop distribution effects. Ice shapes resulting from the bimodal distribution as well as from equivalent monomodal drop size distributions were obtained and compared. Results indicate that the ice shapes resulting from the monomodal and bimodal drop size distributions had similar shapes, but the bimodal distributions had greater mass and volume measurements and icing limits that extended further back on the chord of the model.
Document ID
20190027173
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Potapczuk, Mark G.
(NASA Glenn Research Center Cleveland, OH, United States)
Tsao, Jen-Ching
(Ohio Aerospace Inst. Brook Park, OH, United States)
Date Acquired
July 11, 2019
Publication Date
June 17, 2019
Subject Category
Aeronautics (General)
Report/Patent Number
GRC-E-DAA-TN68067
Meeting Information
Meeting: International Conference on Icing of Aircraft, Engines, and Structures
Location: Minneapolis, MN
Country: United States
Start Date: June 17, 2019
End Date: June 21, 2019
Sponsors: SAE International
Funding Number(s)
WBS: 147016.03.03.02.13.01
CONTRACT_GRANT: NNC13BA10B
Distribution Limits
Public
Copyright
Public Use Permitted.
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