CONDITIONS FOR THE OCCURRENCE OF ICING ON AERODYNAMIC PROFILES AND METHODS OF THEIR CALCULATION

Sungat Berkinovich Akhazhanov, Sergey Skorobogatov

2021

Full text Open access: Gold Metadata (CSL-JSON)

DOI 10.55452/1998-6688-2021-18-2-20-25

Data confidence 70 medium

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Abstract

This article analyzes the methods and models suitable for studying the icing of the aerodynamic surface (wing). Systems to counteract the unifying effect are considered. Methods and models for calculating ice formations on aerodynamic surfaces are studied. Further study of the effect of icing will be conducted in the light of the characteristics of flow around bodies of viscous compressible medium in terms of load and liquid phase in case of changes in the geometric parameters of the bodies and reflect this change in the external stream.