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ISSN: 1064-2285 Print
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DOI: 10.1615/HeatTransRes.v38.i2
Pages: 105
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DOI: 10.1615/HeatTransRes.v38.i2.50
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Article price - $70.00 |
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Ratio of the Thermal and Erosion Components in Heat-Erosion Destruction of Materials in a Supersonic Heterogeneous Flow
D. S. Mikhatulin
Institute of High Temperatures of the Russian Academy of Science, Moscow, Russia, 127412
Yu. V. Polezhaev
Institute for High Temperatures of the Russian Academy of Sciences Moscow, Russia
ABSTRACT
We consider the possibilities for modeling heat-erosion impact of a dusty atmosphere on the elements of the frontal surfaces of rockets on ground-based gasdynamic test benches, which should be reproduced in experimental investigations. A model of heat-erosion destruction of coating materials, in which the total entrainment of mass is divided into thermal, erosion, and gas-mechanical, is proposed. The conditions, when these components are independent of each other and when this dependence can be ignored, are analyzed. The determining parameters are formulated.
pages 143-162
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