Volume 6, Issue 5 No AccessThermal analysis of engine inlet anti-icing systemsKamel M. Al-Khalil, Theo G. Keith Jr., Kenneth J. DeWitt, James K. Nathman and Donald A. DietrichKamel M. Al-Khalil University of Toledo, Toledo, Ohio 43606Search for more papers by this author, Theo G. Keith Jr. University of Toledo, Toledo, Ohio 43606Search for more papers by this author, Kenneth J. DeWitt University of Toledo, Toledo, Ohio 43606Search for more papers by this author, James K. Nathman Analytical Methods, Inc., Redmond, Washington 98052Search for more papers by this author and Donald A. Dietrich General Electric Company, Cincinnati, Ohio 45215Search for more papers by this authorPublished Online:23 May 2012https://doi.org/10.2514/3.23264SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About Previous article Next article FiguresReferencesRelatedDetailsSee PDF for referencesCited byNumerical Simulation and Meta Model of Rotorcraft Electrothermal Ice Protection Systems12 December 2023Experimental Investigation on Ice Accretion Upon Ice Particle Impacting onto Heated SurfaceHaiyang Hu , Linchuan Tian and Hui Hu 16 March 2023 | AIAA Journal, Vol. 61, No. 7Experimental Evaluation of Fatigue Strength of AlSi10Mg Lattice Structures Fabricated by AM25 April 2023 | Aerospace, Vol. 10, No. 5Thermal Feature Analysis of a New Hot-Air Anti-Icing Structure20 February 2023 | Journal of Thermal Science, Vol. 32, No. 3Investigating effects of different anti-icing parameters on gas turbine air intake ice formation24 January 2023 | Journal of Thermal Analysis and Calorimetry, Vol. 23Numerical Simulation and Meta Model of Rotorcraft Electrothermal Ice Protection Systems9 April 2023In-Flight Gas Turbine Engine Icing: ReviewEdem Tetteh , Eric Loth, Martin O. 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Zhao15 April 2016 | Journal of Propulsion and Power, Vol. 32, No. 3Thermal Analysis and Testing of Nonrotating Cone with Hot-Air Anti-Icing SystemW. Dong, J. Zhu, M. Zheng and Y. Chen12 February 2015 | Journal of Propulsion and Power, Vol. 31, No. 3Numerical and Experimental Investigation of Ice Accretion on Rotorcraft Engine Air IntakeG. B. Ahn, K. Y. Jung, R. S. Myong, H. B. Shin and W. G. Habashi24 February 2015 | Journal of Aircraft, Vol. 52, No. 3Numerical Simulation of Hot Air Anti-icing Charateristics of an Aero-engine StrutWei Dong, Jianjun Zhu, Guilin Lei and Mei Zheng3 January 2015Heat Transfer and Temperature Analysis of an Aeroengine Strut Under Icing ConditionsW. Dong, J. Zhu, Zhixiang Zhou and X. Chi5 February 2015 | Journal of Aircraft, Vol. 52, No. 1Thermal Analysis and Testing of a Cone with Leading Edge Hot Air Anti-icing SystemWei Dong, Jianjun Zhu and Mei Zheng10 January 2014Investigation of the Performance of Anti-Icing System of a Rotorcraft Engine Air IntakeJournal of the Korean Society for Aeronautical & Space Sciences, Vol. 41, No. 4Computational and Experimental Investigation of Ice Accretion on the Surface of Rotorcraft Air Intake Anti-Icing SystemGook Bin Ahn, Ki Young Jung, Rho Shin Myong, Hoon Bum Shin and Wagdi Habashi5 January 2013Critical Design Points for the Wing Anti-Icing SystemYongfeng Zhu, Wangchao Han, Hongliang Chang and Sijun Zhang5 January 2013COMPUTATIONAL PREDICTION OF ICE ACCRETION AROUND A ROTORCRAFT AIR INTAKEJournal of computational fluids engineering, Vol. 17, No. 2Numerical Simulation Analysis of a Guide Vane Hot Air Anti-icing SystemWei Dong, Jian Zhu and Qiu Zhao14 June 2012Heat and mass transfer during ice accretion on aircraft wings with an improved roughness modelInternational Journal of Thermal Sciences, Vol. 45, No. 6Solution for Aircraft Anti-Icing System Simulation by a Modified Perturbation Method Sumio Kato 22 May 2012 | Journal of Aircraft, Vol. 43, No. 2New Roughness Computation Method and Geometric Accretion Model for Airfoil Icing Guy Fortin , Adrian Ilinca , Jean-Louis Laforte and Vincenzo Brandi 22 May 2012 | Journal of Aircraft, Vol. 41, No. 1Validation of NASA thermal ice protection computer codes. III - The validation of ANTICEKamel Al-Khalil, Charles Horvath, Dean Miller, William Wright, Kamel Al-Khalil, Charles Horvath, Dean Miller and William Wright22 August 2012New Concept in Runback Water Modeling for Anti-Iced Aircraft Surfaces Kamel M. Al-Khalil , Theo G. Keith Jr. and Kenneth J. De Wittt 22 May 2012 | Journal of Aircraft, Vol. 30, No. 1 What's Popular Volume 6, Number 5September 1990 Metrics Crossmark TopicsConvectionCooling TechnologyEnthalpyGas LawsHeat ConductionHeat TransferHeating, Ventilating, and Air ConditioningMass TransferThermal Modeling and AnalysisThermodynamic PropertiesThermodynamicsThermophysics and Heat Transfer KeywordsAnti Icing SystemEngine InletThermal AnalysisHeat Transfer CoefficientsAerodynamic ForceFlow ConditionsConductionPressure CoefficientNacellesIcing ConditionsDigital Published online23 May 2012