Problems on scientific and methodical maintenance of development and operation of heat-protective coatings for heat-stressed elements of space-rocket engineering. I. Mathematical simulation of processes of the destruction of heat-protective materials
|1Timoshenko, VI, 2Frolov, GA |
1Institute of Technical Mechanics of the National Academy of Sciences of Ukraine and the State Space Agency of Ukraine, Dnipropetrovsk, Ukraine
2I.N. Frantsevich Institute for Material Science Problems, NAS of Ukraine, Kyiv, Ukraine
|Kosm. nauka tehnol. 2003, 9 ;(2-3):034-044|
|Publication Language: Russian|
We give the general characteristic of the problem on modelling of flow of surfaces from heat-protective materials which enter into thermochemical interaction with a gas flow by a high-enthalpy gas flow. Particular attention is given to the mathematical simulation of the interaction of a high-temperature gas flow with heat-protective coatings at hypersonic speeds and to the illustration of main features of flow of bodies under conditions of thermochemical destruction of a heat-protective coating.
|Keywords: heat-protective coatings, mathematical simulation, space-rocket engineering|
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