Thermal protection of aircraft units using film cooling with regard to unsteady heat conductivity

Thermal protection of aircraft units using film cooling with regard to unsteady heat conductivity

A simplified physical and mathematical model of combined thermal conductivity and filtering of a cooler with a strong dependence of dynamic viscosity on temperature during film cooling of bodies was developed. The model takes into account the inflow of the cooler into the gas-dynamic boundary layer...

Full description

Bibliographic Details
Main Authors: Lev N. RABINSKIY, Olga V. TUSHAVINA
Format: Article
Language:English
Published: National Institute for Aerospace Research “Elie Carafoli” - INCAS 2019-08-01
Series:INCAS Bulletin
Subjects:
high-temperature flow
heat and mass transfer
aircraft
mathematical model
heat flow
gaseous coolers
Online Access:http://bulletin.incas.ro/files/rabinskiy_tushavina__vol_11_special_issue.pdf

Similar Items

Similar Items