Study of Heatproof Materials in Nonsteady-State Operating Conditions,
Abstract
The present paper deals with the problem of transient heating and abalation of heat-proof coatings of flight vehicles. An analysis is made of the effect of transient parameters on the characteristics of hypersonic ablation and heating of glassy coatings. An implicit finite-difference procedure of calculation of unsteady thermal conditions at the boundary of a plate whose properties are dependent on temperature is presented. (Modified author abstract)
Document Details
- Document Type
- Technical Report
- Publication Date
- Apr 30, 1974
- Accession Number
- AD0780826
Entities
People
- A. A. Ivanov
- A. D. Markin
- B. M. Pankratov
- O. M. Alifanov
Organizations
- National Air and Space Intelligence Center