Supercooled large droplet icing accretion and its unsteady aerodynamic characteristics on high-lift devices
Author:
Affiliation:
1. School of Aeronautics and Astronautics, Shanghai Jiao Tong University, Shanghai, China
2. J.C.Wu Center of Aerodynamics, Shanghai Jiao Tong University, Shanghai, China
Publisher
SAGE Publications
Subject
Mechanical Engineering,Aerospace Engineering
Link
http://journals.sagepub.com/doi/pdf/10.1177/0954410017706991
Reference11 articles.
1. Development and Theoretical Analysis of an Aircraft Supercooled Icing Model
2. Eulerian Modeling of Supercooled Large Droplet Splashing and Bouncing
3. Character and stability of a wind-driven supercooled water film on an icing surface—I. Laminar heat transfer
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1. Research on Icing Classification Method Based on Wind Tunnel Test with Double Impact Surface Probe;Journal of Physics: Conference Series;2024-01-01
2. Investigation of Icing Effects on Aerodynamic Performance for the High-Lift Configuration of Civil Aircraft;2021 12th International Conference on Mechanical and Aerospace Engineering (ICMAE);2021-07-16
3. Wetting and icing of surfaces;Current Opinion in Colloid & Interface Science;2021-06
4. Large-eddy simulations of complex aerodynamic flows over multi-element iced airfoils;Aerospace Science and Technology;2021-02
5. Study on vortex shedding mode on the wake of horn/ridge ice contamination under high-Reynolds conditions;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2019-03-19
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