journal article·2012-11

Non-destructive investigation of quasi-static indentation damage to C/SiC composites and its effects on compressive properties

H Mei, H Q Li, J X Tao, L F Cheng

Advances in Applied Ceramics· Volume 111· Issue 8
Publisher page

Abstract

AbstractImpact damage was introduced into C/SiC composites by a quasi-static indentation method. Damages with different indentation depths were detected by non-destructive testing (NDT) technologies of thermography, X-ray radiography and ultrasonic C scan, and then the detection resolutions were compared. Effects of the impact damages on the retained compressive strengths of the C/SiCs were investigated. Results indicate that when the indentation depth is <0·5 mm, the C/SiCs reveal the linear elastic behaviour with invisible damage for three NDT methods. Once the indentation depth is >0·75 mm, thermal images and ultrasonic C scan are able to detect the obvious damage, while X-ray radiography did not detect any damage up to the indentation depth of 1·5 mm. The retained compressive strengths decreased gradually with increasing indentation depth, and the descent rate of the compressive strength suddenly increased when the indentation depth is >1·5 mm.
Source: openalex_inverted_index · Quality: baseline

Research context

OpenAlex topics: Advanced ceramic materials synthesis · Metal and Thin Film Mechanics · Advanced materials and composites

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

References (16)

Show source-provided references
1. 10.1016/S0921-5093(98)01079-X10.1016/S0921-5093(98)01079-X ↗
2. 10.1179/174367608X32404510.1179/174367608X324045 ↗
3. 10.1179/174367608X26329610.1179/174367608X263296 ↗
4. 10.1179/174367606X14666710.1179/174367606X146667 ↗
5. 10.1111/j.1151-2916.1999.tb02004.x10.1111/j.1151-2916.1999.tb02004.x ↗
6. 10.1111/j.1151-2916.1999.tb02005.x10.1111/j.1151-2916.1999.tb02005.x ↗
7. 10.1179/174367608X37856910.1179/174367608X378569 ↗
8. 10.1111/j.1744-7402.2007.02153.x10.1111/j.1744-7402.2007.02153.x ↗
9. 10.1016/j.msea.2007.04.06610.1016/j.msea.2007.04.066 ↗
10. Dost EF, Avery WB, Finn LB, Dcewicz LB, Scholz DB, Wishart RE: ‘Impact damage resistance of composite fuselage structure. Part 3’, Proc. 4th ACT Conf., Salt Lake City, UT, USA, June 1993, Boeing Commercial Airplane Group, 759–787.
11. National Research Council: ‘New materials for next-generation commercial transport’ ; 1996, Washington, DC, National Academy Press, 67–70.
12. Poe CC: ‘Mechanics methodology for textile preform composite materials’, Proc. 28th Int. Technical Conf., November 1996, Seattle, WA, USA, SAMPE, 324–338.
13. Shen Z · Acta Mater. Compos. Sin. · 2008 · 25 · 125
14. ‘Standard test method for measuring the damage resistance of a fiber reinforced polymer matrix composite to a drop-weight impact event’, ASTM D 7136-07, ASTM, West Conshohocken, PA, USA, 2007.
15. 10.1016/j.msea.2007.09.05310.1016/j.msea.2007.09.053 ↗
16. 10.1016/j.compscitech.2011.05.01310.1016/j.compscitech.2011.05.013 ↗