The nonstationary problem of thermal conductivity in a two-layer thermal protection coating is under consideration. The solution is given for a metal hemispherical shell with axisymmetrical distribution of the heat flux density over the outer surface of the coating.
Heating of Two-Layer Thermal Protection Coating at Hypersonic Flow around a Spherical Blunting
Russ. Aeronaut.
Russian Aeronautics ; 64 , 1 ; 87-96
2021-01-01
10 pages
Article (Journal)
Electronic Resource
English
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