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Experimental Measurement of Frozen and Partially Melted Water Droplet Impact DynamicsHigh-speed video of single frozen water droplets impacting a surface was acquired. The droplets diameter ranged from 0.4 mm to 0.9 mm and impacted at velocities ranging from 140 m/sec to 309 m/sec. The techniques used to freeze the droplets and launch the particles against the surfaces is described in this paper. High-speed video was used to quantify the ice accretion area to the surface for varying impact angles (30 deg, 45 deg, 60 deg), impacting velocities, and break-up angles. An oxygen /acetylene cross-flow flame used to ensure partial melting of the traveling frozen droplets is also discussed. A linear relationship between impact angle and ice accretion is identified for fully frozen particles. The slope of the relationship is affected by impact speed. Perpendicular impacts, i.e. 30 deg, exhibited small differences in ice accretion for varying velocities, while an increase of 60% in velocity from 161 m/sec to 259 m/sec, provided an increase on ice accretion area of 96% at an impact angle of 60 deg. The increase accretion area highlights the importance of impact angle and velocity on the ice accretion process of ice crystals. It was experimentally observed that partial melting was not required for ice accretion at the tested velocities when high impact angles were used (45 and 60 deg). Partially melted droplets doubled the ice accretion areas on the impacting surface when 0.0023 Joules were applied to the particle. The partially melted state of the droplets and a method to quantify the percentage increase in ice accretion area is also described in the paper.
Document ID
20150002345
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Palacios, Jose
(Pennsylvania State Univ. University Park, PA, United States)
Yan, Sihong
(Pennsylvania State Univ. University Park, PA, United States)
Tan, Jason
(General Electric Co. Niskayuna, NY, United States)
Kreeger, Richard E.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
March 3, 2015
Publication Date
June 16, 2014
Subject Category
Aeronautics (General)
Air Transportation And Safety
Report/Patent Number
GRC-E-DAA-TN14978
Report Number: GRC-E-DAA-TN14978
Meeting Information
Meeting: AIAA/CEAS Aeroacoustics Conference
Location: Atlanta, GA
Country: United States
Start Date: June 16, 2014
End Date: June 20, 2014
Sponsors: American Inst. of Aeronautics and Astronautics, Confederation of European Aerospace Societies
Funding Number(s)
CONTRACT_GRANT: NNX12AK16A
WBS: WBS 648987.02.02.04.20
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Impact Dynamics
Icing
Engine
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