Volume 25, Issue 3 No AccessHeat Transfer Through a Single Hole Bias Flow Acoustic LinerAnthony O. Ives, Jian Wang, Srinivasan Raghunathan and Patrick SloanAnthony O. Ives Queen’s University Belfast, Belfast, Northern Ireland BT7 1NN, United KingdomSearch for more papers by this author, Jian Wang Queen’s University Belfast, Belfast, Northern Ireland BT7 1NN, United KingdomSearch for more papers by this author, Srinivasan Raghunathan Queen’s University Belfast, Belfast, Northern Ireland BT7 1NN, United KingdomSearch for more papers by this author and Patrick Sloan Bombardier Aerospace, Belfast, Northern Ireland BT3 9DZ, United KingdomSearch for more papers by this authorPublished Online:6 Sep 2013https://doi.org/10.2514/1.T3637SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookXLinked InRedditEmail About Previous article Next article FiguresReferencesRelatedDetailsSee PDF for referencesCited byIntegrating Ice Protection and Noise Abatement Systems for Aircraft Application: A Review8 September 2023 | Pertanika Journal of Science and Technology, Vol. 31, No. 6Experimental study on aerodynamic performance of nacelle lip-skin bias flow11 April 2020 | Journal of Mechanical Science and Technology, Vol. 34, No. 4Effect of nozzle rotation angles and sizes on thermal characteristic of swirl anti-icing14 September 2018 | Journal of Mechanical Science and Technology, Vol. 32, No. 9 What's Popular Volume 25, Number 3July 2011 Metrics Crossmark TopicsAerodynamicsAerospace SciencesBoundary LayersComputational Fluid DynamicsExperimental Fluid DynamicsFlow MeasurementFlow RegimesFluid DynamicsFluid Flow PropertiesNumerical AnalysisTurbulenceTurbulence ModelsVortex DynamicsWind Tunnels KeywordsCalculated Heat Transfer CoefficientsThermal ConductionInternal FlowsThermocouplesLow Speed Wind TunnelNumerical ModelingFreestream VelocityHoneycomb StructuresK Epsilon Turbulence ModelTurbulence IntensityDigital Published online6 September 2013