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某型飞行器表面热防护涂料的性能改进研究

李晓升

航空材料学报2011,Vol.31Issue(z1):151-154,4.
航空材料学报2011,Vol.31Issue(z1):151-154,4.

某型飞行器表面热防护涂料的性能改进研究

Study of Improving Thermal Protection Coating's Performance

李晓升1

作者信息

  • 1. 中国空空导弹研究院,河南,洛阳,471009
  • 折叠

摘要

Abstract

The application of thermal protection paint is one of the important measures to protect the air to air missile's cabin and components when subject to aerodynamic heating. When the cabin tested in wind tunnel, thermal protection coating's surface becomes car-bonation, rough and cracked. By reducing the degree of fineness and changing the spraying method, cracks disappear and roughness decreases, and the coating's thermal insulation increase.

关键词

热防护涂层/风洞实验/涂料细度/龟裂/隔热效果

Key words

thermal protection paint/wind tunnel tests/degree of fineness/rough and cracked/thermal insulation

引用本文复制引用

李晓升..某型飞行器表面热防护涂料的性能改进研究[J].航空材料学报,2011,31(z1):151-154,4.

航空材料学报

OA北大核心CSCDCSTPCD

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