Abstract For spherical layer of insulation surface, we give a solution of the linear time-dependent heat transfer problem with axially symmetric distribution of the heat flux density over the layer exterior surface. The insulation material has anisotropic heat conduction properties characterized by the ratio of the thermal conductivities along and across the layer. The solution obtained is used for qualitative estimate of the effect of this ratio on the leveling of temperature distributions for non-uniform heating specific for conditions of an axially symmetric hypersonic flow past a hemispherical blunting.
Heating of an Anisotropic Insulation Layer with Hypersonic Flow Past a Spherical Blunting
Russian Aeronautics ; 62 , 1
2019
Aufsatz (Zeitschrift)
Englisch
Lokalklassifikation TIB: | 770/7040/8000 | |
BKL: | 55.50 Luftfahrzeugtechnik |
Heating of an Anisotropic Insulation Layer with Hypersonic Flow Past a Spherical Blunting
Springer Verlag | 2019
|Heating of Two-Layer Thermal Protection Coating at Hypersonic Flow around a Spherical Blunting
Springer Verlag | 2021
|Laminar turbulent transition at hypersonic speeds: the effects of nose blunting
British Library Online Contents | 1995
|Laminar turbulent transition at hypersonic speeds: the effects of nose blunting
British Library Conference Proceedings | 1995
|Magneto hypersonic boundary-layer flow past a plate.
AIAA | 1967
|