No AccessResults from SLD Mass Loss Tests in the ACT Luton Icing Research Wind TunnelRoger Gent, James Ford, Richard Moser and Dean MillerRoger GentQinetiQSearch for more papers by this author, James FordQinetiQSearch for more papers by this author, Richard MoserQinetiQSearch for more papers by this author and Dean MillerNASA Glenn Research CenterSearch for more papers by this authorSession: AE-5: Supercooled Large Droplet Icing StudiesPublished Online:11 Nov 2012https://doi.org/10.2514/6.2003-389SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookXLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byA two-dimensional splashing model for investigating impingement characteristics of supercooled large droplets1 Apr 2016 | International Journal of Multiphase Flow, Vol. 80Multi-Stepping Ice Prediction on Cylinders and Other Relevant GeometriesPatrick G. Verdin and Jean P. F. Charpin28 May 2013 | Journal of Aircraft, Vol. 50, No. 3Parametric Experiment of Large Droplet Dynamics24 September 2007Effects of Large Droplet Dynamics on Airfoil Impingement CharacteristicsS. Tan21 June 2012Further Application of the Mass Loss Model to the GLC-305 and MS(1)-317 Airfoils20 April 2004Residual Droplet Impacts and Thin Film DynamicsAlric Rothmayer and Joshua Krakos21 June 2012Update On SLD Engineering Tools Development16 June 2003SLD Research in the UK16 June 2003 What's Popular 41st Aerospace Sciences Meeting and Exhibit 06 January 2003 - 09 January 2003Reno, Nevadahttps://doi.org/10.2514/6.2003-389 Crossmark TopicsAerodynamicsAeronauticsAerospace SciencesAirspeedAviationAviation SafetyAviation Weather HazardsFluid DynamicsWind Tunnels KeywordsIcing Wind TunnelSuper Cooled Large DropletsSignal GeneratorIcing ConditionsAcoustic ImpedanceFreestream VelocityAirspeedResonant FrequenciesMass Flow RateSpray NozzlesDigital Submission Topic Aerospace Systems, Operations and Life Cycle