Abstract We present a mathematical model, worked out on the basis of the law of binder composite material (CM) decomposition suggested by authors for numerical solution of the heat and mass transfer problems in the heat protective CM under conditions of aero-gas-dynamic heating. The model makes it possible not to consider hard-realizable chemical kinetics of the binder decomposition and can practically be applied to any CM under high temperature conditions. Numerical examples are given.
Simulation of heat and mass transfer in composite heat protective materials under high temperature conditions
Russian Aeronautics (Iz VUZ) ; 55 , 1 ; 41-49
2012-01-01
9 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
COMPOSITE FOR HEAT TRANSFER WITH HIGH-TEMPERATURE RESISTANCE
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