Energy absorption of composite plates and tubes

被引:18
作者
Dubey, DD [1 ]
Vizzini, AJ [1 ]
机构
[1] Univ Maryland, Dept Aerosp Engn, Composites Res Lab, College Pk, MD 20742 USA
关键词
D O I
10.1177/002199839803200204
中图分类号
TB33 [复合材料];
学科分类号
摘要
A total of 28 graphite/epoxy nat-plate specimens and six graphite/epoxy tube specimens ere crushed under quasi-static conditions to provide a basis far comparison of the measured energy absorbency of these two geometries. The energy absorbency of each specimen was measured, and the specific sustained crushing stress (SSCS) was determined. All plate and tube specimens were manufactured from AS4/3501-6 graphite/epoxy with the same layup and thickness. thus providing a common laminate for comparison. Flat-plate specimens of two different widths were tested to determine the effect of the testing fixture on the observed energy absorbency. The flat-plate results indicate that the specific energy absorbency per unit thickness is nearly independent of the specimen width, with a small contribution to the energy absorbency by the testing fixture. However, this calculated value of measured energy absorption due to the test fixture is within the scatter of the data. The results also indicate that specimen geometry affects specimen stability and therefore the failure modes exhibited by the specimen during crushing. Similar failure modes were observed in the tube and flat-plate specimens with the flat plates absorbing 12% less energy per unit mass. Consequently, flat-plate specimens can be used as a lower-cost alternative to tube specimens or in test programs requiring simpler geometries.
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页码:158 / 176
页数:19
相关论文
共 8 条
[1]   ENERGY-ABSORPTION OF COMPOSITE-MATERIALS [J].
FARLEY, GL .
JOURNAL OF COMPOSITE MATERIALS, 1983, 17 (03) :267-279
[2]  
FARLEY GL, 1987, P 43 AM HEL SOC ANN, P613
[3]   The energy absorption of composite plates under off-axis loads [J].
Fleming, DC ;
Vizzini, AJ .
JOURNAL OF COMPOSITE MATERIALS, 1996, 30 (18) :1977-1995
[4]  
FLEMING DC, 1993, J AM HELICOPTER SOC, V17, P38
[5]   A UNIFIED APPROACH TO PROGRESSIVE CRUSHING OF FIBER-REINFORCED COMPOSITE TUBES [J].
HULL, D .
COMPOSITES SCIENCE AND TECHNOLOGY, 1991, 40 (04) :377-421
[6]   SCALING OF ENERGY ABSORBING COMPOSITE PLATES [J].
JACKSON, K ;
MORTON, J ;
LAVOIE, JA ;
BOITNOTT, R .
JOURNAL OF THE AMERICAN HELICOPTER SOCIETY, 1994, 39 (01) :17-23
[7]  
LAVOIE JA, 1994, EXPT TECHNIQUES NOV, P23
[8]  
SEN JK, 1985, SAMPE QUART, V17, P29