DocumentCode :
3044301
Title :
The effects of insulation thickness on heat transfer for thermal protection system
Author :
Liu, Shuang ; Zhang, Boming ; Xie, Weihua
Author_Institution :
Center for Composite Mater. & Struct., Harbin Inst. of Technol., Harbin, China
fYear :
2010
fDate :
8-10 June 2010
Firstpage :
392
Lastpage :
397
Abstract :
The effects of insulation thickness are investigated with potential application in thermal protection system of hypersonic and re-entry vehicles. The traditional thermal protection system is modeled by the finite difference approach. Four different thicknesses of insulations´ TPS are studied. The numerical calculation results show that structure temperature decreases as the insulation thickness increases as well as temperature difference increases, however, this effect weakens as the insulation thickness increased.
Keywords :
finite difference methods; heat transfer; insulation testing; thermal management (packaging); finite difference approach; heat transfer; insulation thickness; thermal protection system; Materials; Numerical models; Petroleum;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Systems and Control in Aeronautics and Astronautics (ISSCAA), 2010 3rd International Symposium on
Conference_Location :
Harbin
Print_ISBN :
978-1-4244-6043-4
Electronic_ISBN :
978-1-4244-7505-6
Type :
conf
DOI :
10.1109/ISSCAA.2010.5633253
Filename :
5633253
Link To Document :
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