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Simulation of Fluid Flow and Collection Efficiency for a SEA Inc. Multi-Element Probe and Ice Crystal Detector Using GlennICENumerical simulation results of fluid flow and collection efficiency of the Science Engineering Associates Inc. Multi-Element Probe (Multiwire) and Ice Crystal Detector (ICD) are presented. Fluid flow simulations were conducted using NASA's FUN3D while collection efficiency simulations were conducted using NASA's LEWICE3D software and GlennICE software. For both probes, 3D unsteady flow results were time averaged. Simulations were computed for freestream velocities ranging from 85 to 185 m/s and freestream total pressures of 44.8 and 93.1 kPa. Collection efficiency results were computed for four spherical particle diameter sizes of 5, 20, 50, and 100 µm. GlennICE collection efficiency results for the multiwire were compared with previously published collection efficiency values calculated using LEWICE3D. Numerical collection efficiency results for the Ice Crystal Detector are presented for the first time.
Document ID
20220006657
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Ru-Ching Chen
(Glenn Research Center Cleveland, Ohio, United States)
Christopher Porter
(Glenn Research Center Cleveland, Ohio, United States)
Date Acquired
April 29, 2022
Subject Category
Aerodynamics
Meeting Information
Meeting: AIAA Aviation
Location: Chicago, IL
Country: US
Start Date: June 27, 2022
End Date: July 1, 2022
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 109492.02.03.09.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
Single Expert
Keywords
aircraft, icing, Computational Fluid Dynamics
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