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Bimodal SLD Ice Accretion on a NACA 0012 Airfoil ModelAn initial ice shape database has been created to document ice accretions on a 21-inch chord NACA 0012 airfoil model resulting from an exposure to a Supercooled Large Droplet (SLD) icing cloud with a bimodal droplet 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 measured ice shapes on the same model to connect the current database to previously measured information. Ice shapes resulting from the bimodal distribution as well as from equivalent standard droplet distributions were obtained and compared. Results indicate that the ice shapes resulting from the bimodal droplet distributions had higher mass and volume values than their standard distribution equivalents as well as having icing limits that extended further back on the chord of the model.
Document ID
20190025466
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. Cleveland, OH, United States)
King-Steen, Laura E.
(HX5 Sierra, LLC Cleveland, OH, United States)
Date Acquired
June 1, 2019
Publication Date
June 5, 2017
Subject Category
Aeronautics (General)
Report/Patent Number
GRC-E-DAA-TN42614
Report Number: GRC-E-DAA-TN42614
Meeting Information
Meeting: 2017 AIAA AVIATION Forum
Location: Denver, CO
Country: United States
Start Date: June 5, 2017
End Date: June 9, 2017
Sponsors: American Institute of Aeronautics and Astronautics (AIAA)
Funding Number(s)
WBS: 147016.03.03.02.13.02
CONTRACT_GRANT: NNC15BA02B
CONTRACT_GRANT: NNC13BA10B
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
aircraft icing
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