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Update on the NASA Glenn Propulsion Systems Lab Ice Crystal Cloud Characterization (2015)NASA Glenn's Propulsion Systems Lab (PSL), an altitude engine test facility, was outfitted with a spray system to generate ice crystals. The first ice crystal characterization test occurred in 2012. At PSL, 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 will discuss the recent learning from the previous two calibrations. It will describe some of the 12-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
20170000241
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Van Zante, Judith F.
(NASA Glenn Research Center Cleveland, OH United States)
Bencic, Timothy J.
(NASA Glenn Research Center Cleveland, OH United States)
Ratvasky, Thomas P.
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
January 4, 2017
Publication Date
June 13, 2016
Subject Category
Aircraft Propulsion And Power
Research And Support Facilities (Air)
Meteorology And Climatology
Report/Patent Number
GRC-E-DAA-TN32526
Meeting Information
Meeting: 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
Ice Clouds
Calibration
Engine Icing
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