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Simulation of Fluid Flow and Collection Efficiency for an SEA Multi-element ProbeNumerical simulations of fluid flow and collection efficiency for a Science Engineering Associates (SEA) multi-element probe are presented. Simulation of the flow field was produced using the Glenn-HT Navier-Stokes solver. Three dimensional unsteady results were produced and then time averaged for the collection efficiency results. Three grid densities were investigated to enable an assessment of grid dependence. Collection efficiencies were generated for three spherical particle sizes, 100, 20, and 5 micron in diameter, using the codes LEWICE3D and LEWICE2D. The free stream Mach number was 0.27, representing a velocity of approximately 86 ms. It was observed that a reduction in velocity of about 15-20 occurred as the flow entered the shroud of the probe.Collection efficiency results indicate a reduction in collection efficiency as particle size is reduced. The reduction with particle size is expected, however, the results tended to be lower than previous results generated for isolated two-dimensional elements. The deviation from the two-dimensional results is more pronounced for the smaller particles and is likely due to the effect of the protective shroud.
Document ID
20140011335
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Rigby, David L.
(Vantage Partners, LLC Brook Park, OH, United States)
Struk, Peter M.
(NASA Glenn Research Center Cleveland, OH United States)
Bidwell, Colin
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
September 3, 2014
Publication Date
June 16, 2014
Subject Category
Aircraft Stability And Control
Report/Patent Number
GRC-E-DAA-TN15808
Report Number: GRC-E-DAA-TN15808
Meeting Information
Meeting: AIAA Aviation 2014
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 648987.02.02.03.20
CONTRACT_GRANT: NNC12BA01B
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Aircraft Icing
Water Content
computational fluid dynamics
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