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Further Examinations of Bimodal SLD Ice Accretion in the NASA Icing Research TunnelAn ice shape database has been created to document ice accretions on 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 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 mono-modal drop size distributions were obtained and compared. Results indicate that the ice shapes resulting from the bimodal drop size distributions had higher mass and volume values than their mono-modal distribution equivalents as well as having icing limits that extended further back on the chord of the model.
Document ID
20180006521
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)
Date Acquired
October 18, 2018
Publication Date
June 25, 2018
Subject Category
Air Transportation And Safety
Report/Patent Number
GRC-E-DAA-TN56249
Report Number: GRC-E-DAA-TN56249
Meeting Information
Meeting: AIAA Aviation and Aeronautics Forum and Exposition
Location: Atlanta, GA
Country: United States
Start Date: June 25, 2018
End Date: June 29, 2018
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNC13BA10B
WBS: WBS 147016.03.03.02.13.01
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Aircraft
Icing
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