Author:
Liu Wenfeng,Huang Xiong,Ge Junfeng,Luo Huan
Abstract
Abstract
Facing supercooled large water droplet environment, an effective ice detection method is a prerequisite to implement the avoidance strategy and get out of the icing environment of SLD as soon as possible. Fiber-optic icing sensors were arranged on the double impact surface probe. The probe was used for icing wind tunnel test. Different machine learning algorithms were used to establish the classification method of icing conditions based on multi-sensor ice thickness information fusion. An appropriate algorithm was selected for the classification method to detect icing conditions. The icing classification method based on SVM could effectively distinguish the conventional water droplet icing condition from the SLD icing condition, and it has significant potential on aviation industry application.
Reference24 articles.
1. Aircraft icing: An ongoing threat to aviation safety;Cao;Aerospace Science and Technology,2018
2. Aircraft Icing Analysis of Alternatives;Kreeger;AVIATION Forum,2022
3. Effect of drop size on the impact thermodynamics for supercooled large droplet in aircraft icing;Zhang;Physics of Fluids,2016
4. Supercooled large droplet icing accretion and its unsteady aerodynamic characteristics on high-lift devices;Zhang;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering,2018