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Development of 3D Ice Accretion Measurement MethodIcing wind tunnels are designed to simulate in-flight icing environments. The chief product of such facilities is the ice accretion that forms on various test articles. Documentation of the resulting ice accretion key piece of data in icing-wind-tunnel tests. Number of currently used options for documenting ice accretion in icing-wind-tunnel testing.
Document ID
20130000320
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Lee, Sam (ASRC Aerospace Corp. Cleveland, OH, United States)
Broeren, Andy P. (NASA Glenn Research Center Cleveland, OH, United States)
Addy, Harold E., Jr. (NASA Glenn Research Center Cleveland, OH, United States)
Sills, Robert (Sierra Lobo, Inc. Fremont, OH, United States)
Pifer, Ellen M. (Saint Louis Univ. MO, United States)
Date Acquired
August 27, 2013
Publication Date
June 25, 2012
Subject Category
Aerodynamics
Report/Patent Number
E-18389-1
Report Number: E-18389-1
Meeting Information
Meeting: AIAA Atmospheric and Space Environments Conference
Location: New Orleans, LA
Country: United States
Start Date: June 25, 2012
End Date: June 28, 2012
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 648987.02.03.03.10
Distribution Limits
Public
Copyright
Public Use Permitted.

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