Author:
Amelyushkin I A,Kudrov M A,Kuleshov P S
Abstract
Abstract
New results of aircraft icing are obtained. New mathematical models of physical phenomena are formulated. Original construction of adaptive wing was invented, developed and prototypes were built. New algorithm of aircrafts’ surface with nanorelief are developed. Parametric studies of aircraft icing peculiarities were carried out.
Reference15 articles.
1. Antiicing performance of superhydrophobic coatings on aluminum and stainless steel;Boinovich;Russian Chemical Bulletin,2013
2. Similarity criteria and peculiarities of ice accretion on bodies in air flows containing supercooled droplets;Amelyushkin;Uchenye Zapiski TsAGI,2023
3. Engineering Flows in Small Devices: Microfluidics toward a Labon-a-Chip;Stone;Annual Review of Fluid Mechanics,2004
4. Breakup dynamics of capillary bridges on hydrophobic stripes;Hartman;International Journal of Multiphase Flow,2023