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Update on the NASA Glenn Propulsion Systems Lab Ice Crystal Cloud Characterization (2015, 2016)NASA Glenn's Propulsion Systems Lab, an altitude engine test facility, was outfitted with a spray system to generate ice crystals in 2011. Turbine engines and driven rigs can experience ice crystal icing at flight altitudes, temperatures and Mach numbers. To support these tests, four ice crystal characterizations have been conducted in two different facility configurations. In addition, super-cooled liquid and mixed phase clouds have also been generated. This paper represents a work in progress. It will describe some of the 11-parameter calibration space, and how those parameters interact with each other, the instrumentation used to characterize the cloud and present a sample of the cloud characterization results.
Document ID
20170002542
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Van Zante, Judith
(NASA Glenn Research Center Cleveland, OH United States)
Bencic, Timothy
(NASA Glenn Research Center Cleveland, OH United States)
Ratvasky, Thomas
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
March 27, 2017
Publication Date
June 13, 2016
Subject Category
Research And Support Facilities (Air)
Aircraft Propulsion And Power
Meteorology And Climatology
Report/Patent Number
GRC-E-DAA-TN32903
Meeting Information
Meeting: AIAA Aviation and Aeronautics Forum and Exposition (AIAA AVIATION 2016)
Location: Washington, DC
Country: United States
Start Date: June 13, 2016
End Date: June 17, 2016
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 432938.11.01.03.05.01.03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Engine Icing
Calibration
Ice Clouds
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