Specimen geometry effects on high-strain-rate testing of graphite/epoxy composites

Citation
E. Woldesenbet et Jr. Vinson, Specimen geometry effects on high-strain-rate testing of graphite/epoxy composites, AIAA J, 37(9), 1999, pp. 1102-1106
Citations number
6
Categorie Soggetti
Aereospace Engineering
Journal title
AIAA JOURNAL
ISSN journal
00011452 → ACNP
Volume
37
Issue
9
Year of publication
1999
Pages
1102 - 1106
Database
ISI
SICI code
0001-1452(199909)37:9<1102:SGEOHT>2.0.ZU;2-S
Abstract
Numerous papers have been published that include high-strain-rate experimen tal data obtained from Split Hopkinson Pressure Bar (SHPB) tests. There hav e been no standardized test specimens with differing dimensions and geometr y. For this reason, it can be difficult to compare results of tests perform ed by other researchers. The SHPB facility was used in this study to determ ine if specimen geometry has an effect on the results of high-strain-rate c ompression tests. The material used in all of the tests is a unidirectional IM7/8551-7 graphite/epoxy composite. The experiments discussed herein show the effect of varying the length-to-diameter (L/D, or aspect) ratio of the specimen, as well as the effect of changing from the more typical cylindri cal to a square/rectangular specimen geometry. The L/D study examined 84 cy lindrical specimens with L/Ds from 0.5 to 2.0, with D=0.261 in., and tested in both the 1 and 2 directions. The geometry study used 42 square/rectangu lar specimens and tested in the 1, 2, and 3 directions. The results of both studies are compared, and no statistically significant effect of either L/ D or geometry could be found.