A CURVED BEAM TEST SPECIMEN FOR DETERMINING THE INTERLAMINAR TENSILE-STRENGTH OF A LAMINATED COMPOSITE

被引:59
作者
HIEL, CC
SUMICH, M
CHAPPELL, DP
机构
[1] NASA-Ames Research Center, Moffett Field, CA 94035
关键词
D O I
10.1177/002199839102500705
中图分类号
TB33 [复合材料];
学科分类号
摘要
A curved beam type of test specimen is evaluated for use in determining the through-the-thickness strength of laminated composites. Two variations of a curved beam specimen configuration (semicircular and elliptical) were tested to failure using static and fatigue loads. The static failure load for the semicircular specimens was found to be highly sensitive to flaw content, with the specimens falling into two distinct groups. This result supports the use of proof testing for structural validation. Static design allowables are derived based on the Weibull distribution. Fatigue data indicates no measured increase in specimen compliance prior to final fracture. All static and fatigue failures at room temperature dry conditions occurred catastrophically. The elliptical specimens demonstrated unusually high failure strengths indicating the presence of phenomena requiring further study. Results are also included for specimens exposed to a wet environment showing a matrix strength degradation due to moisture content. Further testing is underway to evaluate a fatigue methodology for matrix dominated failures based on residual static strength (wearout).
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页码:854 / 868
页数:15
相关论文
共 10 条
[1]   INTERLAMINAR STRESSES IN TAPERED LAMINATES [J].
HOA, SV ;
DAOUST, J ;
DU, BL ;
VUKHANH, T .
POLYMER COMPOSITES, 1988, 9 (05) :337-344
[2]   FLEXURE OF SIMPLY CURVED COMPOSITE SHAPES [J].
KEDWARD, KT ;
WILSON, RS ;
MCLEAN, SK .
COMPOSITES, 1989, 20 (06) :527-536
[3]  
KO WL, 1989, NASA4139 TECHN MEM
[4]  
LAGACE PA, 1986, 2ND ASTM S TEST METH
[5]  
LANE JW, 1987, 1987 SAE INT POW LIF
[6]  
MANDELL JF, 1974, 29TH ANN TECHN C SOC
[7]  
MAO TH, 1982, ASTM STP, V787, P5
[8]  
SUMICH M, 1989, EXPT TECHNIQUES OCT, P20
[9]   IMPACT INDUCED STRESSES, STRAINS, AND DELAMINATIONS IN COMPOSITE PLATES [J].
WU, HYT ;
SPRINGER, GS .
JOURNAL OF COMPOSITE MATERIALS, 1988, 22 (06) :533-560
[10]  
MIL HDB B, V17