宇航材料工艺2011，Vol.41Issue(5)：78-80,3.
复合材料质量烧蚀率计算模型实验研究
Experimental Validation of Calculated Model on Mass Loss Rate of Composites
周燕萍 1魏莉萍 1郑会保 1孟祥艳 1刘运传1
作者信息
- 1. 中国兵器工业集团第五三研究所,济南250031
- 折叠
摘要
Abstract
In this paper, the important characteristic parameter, namely the mass loss rate, was obtained by the investigating on CF/S-157PF composite under oxyacetylene flame test conditions. And using multiple linear regression , the mathematic model on the mass loss rate and the two major factors, namely the heat flux density and ablation time is as follows; M = 0. 043 · q0.128 · t-0.191 . It is verified that, the regression model is very applicable and the forecast accuracy is much better. So the erosion properties of CF/S-157PF composite can be evaluated with this rapid, effective, and accurate method in the oxyacetylene flame test.关键词
氧-乙炔烧蚀/多元回归/热流密度/质量烧蚀率/数学模型Key words
Oxyacetylene flame/Multiple regression/Heat flux density/Mass loss rate/Mathematic model引用本文复制引用
周燕萍,魏莉萍,郑会保,孟祥艳,刘运传..复合材料质量烧蚀率计算模型实验研究[J].宇航材料工艺,2011,41(5):78-80,3.
