Deformation and failure of alumina under high strain rate compressive loading

被引:50
作者
Acharya, Saikat [1 ]
Bysakh, Sandip [2 ]
Parameswaran, Venkitanarayanan [3 ]
Mukhopadhyay, Anoop Kumar [4 ]
机构
[1] CSIR, Cent Glass & Ceram Res Inst, Nonoxide Ceram & Composite Div, Kolkata 700032, India
[2] CSIR, Cent Glass & Ceram Res Inst, Nano Struct Mat Div, Kolkata 700032, India
[3] Indian Inst Technol, Dept Mech Engn, Kanpur 208016, Uttar Pradesh, India
[4] CSIR, Cent Glass & Ceram Res Inst, Adv Mech & Mat Characterizat Div, Kolkata 700032, India
关键词
Alumina; SHPB; Strain rate; Compressive strength; Microcracks; SHEAR LOCALIZATION; BRITTLE MATERIALS; IMPACT DAMAGE; SHOCK; CERAMICS; STRENGTH; FRAGMENTATION; INDENTATION; PLASTICITY; ARMOR;
D O I
10.1016/j.ceramint.2015.01.126
中图分类号
TQ174 [陶瓷工业]; TB3 [工程材料学];
学科分类号
0805 ; 080502 ;
摘要
For development of structural ceramics e.g., alumina for high strain rate resistant applications, it is extremely important to understand the issues involved in compressive microfracture and the role of compressive microfracture in the global failure process at high strain rates. Thus the present work reports compressive strength of a dense (e.g., rho similar to 97.2% P-th) 5 mu m grain size alumina exposed to high strain rate (e.g., 0.9 x 10(3) s(-1)) loading in SHPB experiments. Concomitant utilization of high-speed videography has been exploited to study in-situ the details of the dynamic fragmentation process. The maximum compressive strength is measured to be similar to 3 GPa. Post-mortem examination of the recovered alumina fragments has been performed by FESEM and TEM. Apart from conventional global brittle fracture, the results show the grain localized microcleavages, intragranular microcracking, plasticity, dislocations as well as formation of subgrain structure to occur in alumina Based on these experimental results the reasons of compressive microfracture and its probable role in the global failure process of alumina ceramic are discussed. (C) 2015 Elsevier Ltd and Techna Group S.r.l. All rights reserved.
引用
收藏
页码:6793 / 6801
页数:9
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