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Ice Particle Impacts on a Moving WedgeThis work presents the results of an experimental study of ice particle impacts on a moving wedge. The experiment was conducted in the Adverse Environment Rotor Test Stand (AERTS) facility located at Penn State University. The wedge was placed at the tip of a rotating blade. Ice particles shot from a pressure gun intercepted the moving wedge and impacted it at a location along its circular path. The upward velocity of the ice particles varied from 7 to 12 meters per second. Wedge velocities were varied from 0 to 120 meters per second. Wedge angles tested were 0 deg, 30 deg, 45 deg, and 60 deg. High speed imaging combined with backlighting captured the impact allowing observation of the effect of velocity and wedge angle on the impact and the post-impact fragment behavior. It was found that the pressure gun and the rotating wedge could be synchronized to consistently obtain ice particle impacts on the target wedge. It was observed that the number of fragments increase with the normal component of the impact velocity. Particle fragments ejected immediately after impact showed velocities higher than the impact velocity. The results followed the major qualitative features observed by other researchers for hailstone impacts, even though the reduced scale size of the particles used in the present experiment as compared to hailstones was 4:1.
Document ID
20150002344
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Vargas, Mario
(NASA Glenn Research Center Cleveland, OH United States)
Struk, Peter M.
(NASA Glenn Research Center Cleveland, OH United States)
Kreeger, Richard E.
(NASA Glenn Research Center Cleveland, OH United States)
Palacios, Jose
(Pennsylvania State Univ. University Park, PA, United States)
Iyer, Kaushik A.
(Johns Hopkins Univ. Baltimore, MD, United States)
Gold, Robert E.
(Johns Hopkins Univ. Baltimore, MD, 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-TN14983
Report Number: GRC-E-DAA-TN14983
Meeting Information
Meeting: AIAA Atmospheric and Space Environments Conference
Location: Atlanta, GA
Country: United States
Start Date: June 16, 2014
End Date: June 20, 2014
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 648987.02.03.03.20
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Roughness
Icing
Supercooled Drooplets
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