Numerical modeling of gas leakage through damaged composite laminates

被引:25
作者
Kumazawa, Hisashi [1 ]
Whitcomb, John [2 ]
机构
[1] Japan Aerosp Explorat Agcy, Struct Technol Ctr, Mitaka, Tokyo 1810015, Japan
[2] Texas A&M Univ, Dept Aerosp Engn, College Stn, TX 77843 USA
关键词
laminates; leakage; finite element analysis; cracks; delamination; cryogenic tank;
D O I
10.1177/0021998308092210
中图分类号
TB33 [复合材料];
学科分类号
摘要
A computational fluid dynamics (CFD) model was developed to predict leakage through a damaged laminate. Crack opening displacements (COD) from a 3D finite element model were fit using a polynomial function. This curve fit was then used in defining the openings in the CFD model. Delamination length at crack intersections was estimated based on experimental data for specimens subjected to thermal loads only. Leakage under combined thermal and biaxial mechanical loadings was predicted with the estimated delamination length. Considering the sensitivity of the predictions to many variables, the calculated leakage under combined thermal and biaxial mechanical loadings was estimated with reasonable accuracy.
引用
收藏
页码:1619 / 1638
页数:20
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