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SIMPLIFICATION OF A KIND OF COMPOSITE STRUCTURE

DOI: 10.1615/ICHMT.2017.CHT-7.610
pages 627-631

Bo Chen
CAS Key Laboratory of Microwave Remote Sensing, National Space Science Center, Chinese Academy of Sciences, Beijing 100190, China; College of Materials Science and Opto-Electronic Technology, University of Chinese Academy of Sciences, Beijing, 101408, China

Ning Li
Key laboratory of microwave remote sensing, Chinese Academy of Sciences, Beijing, 100190, China; National Space Science Center, Chinese Academy of Sciences, Beijing, 100190, China

要約

In this paper, the thermal simplification of surface of a satellite borne microwave antenna of a kind of sandwich composite of carbon fiber and Aluminum honeycomb is discussed. To this kind of composite it is needed to do some simplification when doing the thermal analysis. A uniform unit repeatedly was gotten and the equivalent thermal parameters such as thermal conductivity and heat capacity were computed. The influences of simplification methods to the thermal results and compute speed were contracted and discussed.

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