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• W2561420211 abstract "No AccessTechnical NoteHeat Transfer Evaluation on Ice-Roughened CylindersYiqiang Han and Jose PalaciosYiqiang HanClemson University, Clemson, South Carolina 29642*Lecturer, Department of Mechanical Engineering; . Member AIAA.Search for more papers by this author and Jose PalaciosPennsylvania State University, University Park, Pennsylvania 16802†Assistant Professor, Department of Aerospace Engineering; . Member AIAA.Search for more papers by this authorPublished Online:29 Dec 2016https://doi.org/10.2514/1.J055218SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Hansman R., Yamaguchi K., Berkowitz B. and Potapczuk M., “Modeling of Surface Roughness Effects on Glaze Ice Accretion,” 27th Aerospace Sciences Meeting, AIAA Paper 1989-0734, Jan. 1989. LinkGoogle Scholar[2] Achenbach E., “Total and Local Heat Transfer from a Smooth Circular Cylinder in Cross-Flow at High Reynolds Number,” International Journal of Heat and Mass Transfer, Vol. 18, No. 12, 1975, pp. 1387–1396. doi:https://doi.org/10.1016/0017-9310(75)90252-5 IJHMAK 0017-9310 CrossrefGoogle Scholar[3] Achenbach E., “The Effect of Surface Roughness on the Heat Transfer from a Circular Cylinder to the Cross Flow of Air,” International Journal of Heat and Mass Transfer, Vol. 20, No. 4, 1977, pp. 359–369. doi:https://doi.org/10.1016/0017-9310(77)90157-0 IJHMAK 0017-9310 CrossrefGoogle Scholar[4] Frossling N., “Evaporation, Heat Transfer, and Velocity Distribution in Two-Dimensional and Rotationally Symmetrical Laminar Boundary-Layer Flow,” NACA TM-1432, 1958. Google Scholar[5] Palacios J., Han Y., Brouwers E. and Smith E., “Icing Environment Rotor Test Stand Liquid Water Content Measurement Procedures and Ice Shape Correlation,” Journal of American Helicopter Society, Vol. 57, No. 2, 2012, Paper 022006. Google Scholar[6] Han Y. and Palacios J., “Analytical and Experimental Determination of Airfoil Performance Degradation Due to Ice Accretion,” 4th AIAA Atmospheric and Space Environments Conference, AIAA Paper 2012-2794, June 2012. LinkGoogle Scholar[7] Camci C., Kim K., Hippensteele S. A. and Poinsatte P. E., “Convective Heat Transfer at the Curved Bottom Surface of a Square to Rectangular Transition Duct Using a New Hue Capturing Based Liquid Crystal Technique,” ASME Fundamental Experimental Measurements in Heat Transfer-HTD, Vol. 179, 1991, pp. 7–22; also ASME Journal of Heat Transfer (in color), Vol. 115, pp. 311–324. Google Scholar[8] Camci C., Kim K., Hippensteele S. and Poinsatte P., “Evaluation of a Hue Capturing Based Transient Liquid Crystal Method for High-Resolution Mapping of Convective Heat Transfer on Curved Surfaces,” Journal of Heat Transfer, Vol. 115, No. 2, 1993, pp. 311–318. doi:https://doi.org/10.1115/1.2910681 JHTRAO 0022-1481 CrossrefGoogle Scholar[9] Han Y. and Palacios J., “Surface Roughness and Heat Transfer Prediction for Development of an Improved Aircraft Ice Accretion Modeling Tool,” 8th AIAA Atmospheric and Space Environments Conference, AIAA Paper 2016-3589, June 2016. LinkGoogle Scholar Previous article Next article FiguresReferencesRelatedDetailsCited byHeat Transfer Correlations for Smooth and Rough Airfoils13 February 2023 | Fluids, Vol. 8, No. 2Direct numerical simulation of transitional flow past an airfoil with partially covered wavy roughness elementsPhysics of Fluids, Vol. 34, No. 10Engine Inlet Guide Vane Ice Impact FragmentationYiqiang Han, Jared Soltis and Jose Palacios5 June 2018 | AIAA Journal, Vol. 56, No. 9Latent Heat and Liquid Water Content (LWC) Sensor based on Transient Heat Flux MeasurementsYiqiang Han and Jose Palacios24 June 2018 What's Popular Volume 55, Number 3March 2017 CrossmarkInformationCopyright © 2016 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the ISSN 0001-1452 (print) or 1533-385X (online) to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsAerodynamicsAeronautical EngineeringAeronauticsConvectionHeat ConductionHeat TransferThermal MeasurementThermocouplesThermodynamic PropertiesThermodynamicsThermophysical PropertiesThermophysics and Heat TransferWind Tunnels KeywordsCalculated Heat Transfer CoefficientsLow Speed Wind TunnelTransient Heat ConductionStagnation PointThermal PropertiesSurface Mount ThermocouplesHeat Flux SensorIcing ConditionsPolyvinyl ChlorideSurface RoughnessAcknowledgmentsThe authors would like to thank the Vertical Lift Research Center of Excellence and the U.S. Army for sponsoring this research. This research is funded by the Government under agreement number W911W6-11-2-0011. The U.S. Government is authorized to reproduce and distribute reprints notwithstanding any copyright notation thereon. The views and conclusions contained in this document are those of the authors and should not be interpreted as representing the official policies, either expressed or implied, of the U.S. Government.PDF Received22 March 2016Accepted25 September 2016Published online29 December 2016" @default.
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