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Comparing Experimental Ice Accretions on a Swept Wing with 3D Morphogenetic Simulations

2018; American Institute of Aeronautics and Astronautics; Volume: 55; Issue: 6 Linguagem: Inglês

10.2514/1.c034879

1533-3868

Krzysztof Szilder, Edward P. Lozowski,

Aerospace Engineering and Energy Systems

No AccessEngineering NoteComparing Experimental Ice Accretions on a Swept Wing with 3D Morphogenetic SimulationsKrzysztof Szilder and Edward P. LozowskiKrzysztof SzilderNational Research Council, Ottawa, Ontario K1A 0R6, Canada and Edward P. LozowskiUniversity of Alberta, Edmonton, Alberta T6G 2E3, CanadaPublished Online:31 Jul 2018https://doi.org/10.2514/1.C034879SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Vargas M. and Reshotko E., "LWC and Temperature Effects of Ice Accretion Formation on Swept Wings at Glaze Ice Conditions," AIAA Paper 2000-0483, 2000. LinkGoogle Scholar[2] Vargas M., Giriunas J. A. and Ratvasky T. P., "Ice Accretion Formations on a NACA 0012 Swept Wing Tip in Natural Icing Conditions," AIAA Paper 2002-0244, 2002. LinkGoogle Scholar[3] Vargas M., "Current Experimental Basis for Modeling Ice Accretions on Swept Wings," AIAA Paper 2005-5188, 2005. 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TopicsAerodynamicsAeronautical EngineeringAeronauticsAircraft DesignAircraft Operations and TechnologyAircraft Wing DesignAirspeedComputational Fluid DynamicsFlow RegimesFluid DynamicsLattice Boltzmann MethodsNumerical AnalysisWind Tunnels KeywordsSwept WingIcing ConditionsIcing Wind TunnelSurface Heat TransferSweep AngleAircraft IcingCFDLattice Boltzmann MethodsAtmospheric ConditionsNumerical ModelingAcknowledgmentThe second author would like to thank NSERC for a Discovery Grant.PDF Received12 December 2017Accepted11 June 2018Published online31 July 2018