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Numerical and experimental study of flow field characteristics of an iced airfoil
Authors:Masoud Mirzaei  Mohammad A Ardekani  Mehdi Doosttalab
Institution:1. Department of Aerospace, K.N. Toosi University of Technology, 322 Mirdamad Ave. West, 19697, Tehran, Iran;2. Iranian Organization of Science and Technology, No. 71, Forsat St, Ferdousi Sq, Tehran, Iran;3. Department of Aerospace, K.N. Toosi University of Technology, Iran;1. School of Aeronautic Science and Engineering, Beihang University, Beijing 100191, China;2. China Aerospace Science and Industry Corporation, Beijing 100074, China;1. Building Physics and Services, Department of the Built Environment, Eindhoven University of Technology, P.O. Box 513, 5600 MB Eindhoven, The Netherlands;2. Building Physics Section, Department of Civil Engineering, Leuven University, Kasteelpark Arenberg 40 – bus 2447, 3001 Leuven, Belgium;1. Department of Wind Energy, Technical University of Denmark, Denmark;2. School of Mechanical, Electrical and Manufacturing Engineering, Loughborough University, UK;1. Center for Applied Mathematics, Tianjin University, Tianjin, 300072, China;2. School of Aeronautics, Northwestern Polytechnical University, Xi''an, 710072, China;3. State Key Laboratory for Strength and Vibration of Mechanical Structures, Xi''an Jiaotong University, 710049, China;4. General Design and Aerodynamic Department, Xi''an Aircraft Design Institute, Xi''an, 710089, China
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