Moisture Behavior of Aeronautic Carbon Fiber Reinforced Resin Composite Stiffened Panel

被引：1
|
作者：
Tan Xiang-fei [1 ]
Tan Peng-da [2 ]
He Yu-ting [1 ]
Feng Yu [1 ]
An Tao [1 ]
Zhang Tian-yu [1 ]
Liu Kai [1 ]
机构：
[1] Air Force Engn Univ, Aeronaut Engn Coll, Xian 710038, Shaanxi, Peoples R China
[2] Chongqing Nanping Middle Sch, Chongqing 400000, Peoples R China
来源：
CAILIAO GONGCHENG-JOURNAL OF MATERIALS ENGINEERING | 2018年 / 46卷 / 12期
关键词：
composite stiffened panel; moisture behavior; moisture model; moisture concentration distribution;
D O I：
10.11868/j.issn.1001-4381.2017.000728
中图分类号：
T [工业技术];
学科分类号：
08 ;
摘要：
In order to investigate the moisture property of carbon fiber reinforced resin composite stiffened panel in hygrothermal environment, moisture experiments were conducted in condition of 70 degrees C/85%RH. Stage moisture model was proposed and moisture behaviors were analyzed by finite element method. The results show that the moisture curve of experimental result agrees with Fick's diffusion law perfectly in initial moisture stage. However, stage moisture behavior exists in later moisture period. The moisture curve of stage moisture model agrees with finite element result, with an error less than 5% compared with the experimental result. The composite stiffened panel moisture mechanism is revealed by moisture concentration distribution. Additionally, the saturated moisture rate in different thickness zones is not synchronous, which is main reason resulting in stage moisture.
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收藏
页码：61 / 69
页数：9
相关论文
共 19 条
  • [1] American Society for Testing and Materials, 1992, D5229D5229M ASTM
  • [2] Chinese Aeronautical Establishment, 2001, MAN COMP STRUCT DES
  • [3] [冯青 Feng Qing], 2010, [复合材料学报, Acta Materiae Compositae Sinica], V27, P16
  • [4] Feng Tongbo, 2010, Journal of Beijing University of Aeronautics and Astronautics, V36, P1427
  • [5] [高坤 Gao Kun], 2016, [复合材料学报, Acta Materiae Compositae Sinica], V33, P1147
  • [6] Characterization of anisotropic moisture absorption in polymeric composites using hindered diffusion model
    Grace, L. R.
    Altan, M. C.
    [J]. COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2012, 43 (08) : 1187 - 1196
  • [7] On the durability of FRP composites for aircraft structures in hygrothermal conditioning
    Guermazi, Noamen
    Ben Tarjem, Amira
    Ksouri, Imen
    Ayedi, Hassine Ferid
    [J]. COMPOSITES PART B-ENGINEERING, 2016, 85 : 294 - 304
  • [8] Harris G C, 1978, J COMPOS MATER, V12, P118
  • [9] LI L K, 2016, STUDY DEGRADATION CO
  • [10] NAN T T, 2013, INFLUENCE BENDING LO
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