An approach for stress analysis of corrugated-core integrated thermal protection system under thermal and mechanical environment

2018 ◽  
Vol 185 ◽  
pp. 1-26 ◽  
Author(s):  
Chunlin Gong ◽  
Yifan Wang ◽  
Liangxian Gu ◽  
Shengbo Shi
AIAA Journal ◽  
2010 ◽  
Vol 48 (1) ◽  
pp. 119-128 ◽  
Author(s):  
Oscar A. Martinez ◽  
Anurag Sharma ◽  
Bhavani V. Sankar ◽  
Raphael T. Haftka ◽  
Max L. Blosser

2009 ◽  
Vol 46 (3) ◽  
pp. 501-513 ◽  
Author(s):  
Christian Gogu ◽  
Satish K. Bapanapalli ◽  
Raphael T. Haftka ◽  
Bhavani V. Sankar

Author(s):  
D. I. Aronov ◽  
V. V. Klyagin

On the basis of analytical and experimental data, this paper presents possible levels of thermal loading of reusable hypersonic aircrafts. Methods for ensuring the thermal regime of such aircrafts using various passive and active thermal protection technologies are considered. The conducted analysis of the scientific and technical background in terms of the practical implementation of these technologies allowed the authors to draw the conclusion about the relevance and expediency of creating an integrated thermal protection system for reusable high-speed aircrafts.


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