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University of Cambridge

Extraction of mechanical properties over a range of strain rates from indentation data

Abstract

dc:description.abstract

A procedure is described for indentation creep plastometry. It is based on iterative numerical simulation of the indentation process, with repeated comparison between an experimental outcome and the corresponding model prediction, systematically varying the values of parameters in a constitutive law until optimal agreement is achieved. The experimental outcome is the penetration depth as a function of time, under a constant applied load. An important feature of the procedure is the prior creation of a spherical recess in the sample, having a pre-selected depth and a curvature radius equal to that of the indenter. This allows control over the stress levels created during the indentation creep testing and can be used to ensure that no (time-independent) plastic deformation is stimulated during the test. Confirmation of the viability of the procedure is provided via comparisons between the creep characteristics of pure nickel samples at 750˚C, obtained in this way and via conventional uniaxial tensile testing. A similar procedure has been applied for the study of rate-dependent plasticity in bulk metallic materials. Ballistic impact (indentation) of hard spherical projectiles was used to study a rigidly held target, with operative strain rates of the order 105 s-1. Input for the FEM model includes data characterizing the (temperature-dependent) quasi-static plasticity, obtained by conventional uniaxial testing. The experimental outcomes are displacement-time plots for the projectile and the residual indent profile. Since the strain rate sensitivity is characterised by a single parameter value (C in the Johnson–Cook formulation), convergence on its optimum value is straightforward, although a parameter characterizing interfacial friction is also required. Using experimental data from (both work-hardened and annealed) copper samples, this procedure has been carried out and best-fit values of C (∼0.016 and ∼0.030) have been obtained. This procedure has been extended for the study of fracture characteristics (under high imposed strain rates). The strain rate sensitivity of magnesium was evaluated (C~0.026) as above. The main emphasis, however, is on study of its fracture characteristics, with tomographic imaging being used to obtain crack patterns for different projectile velocities. An approach based on fracture mechanics, and on use of FEM modelling to estimate the strain energy release rate required for crack propagation (i.e. the fracture energy of the material) is proposed and applied to these experimental results, leading to a value of the order of 2 kJ m-2. While such a procedure is unlikely to produce accurate values, partly because the crack propagation takes place under local conditions that change rapidly and are not well-defined, this figure is plausible for the case concerned. While there are several sources of complexity, it may be possible to develop this methodology, both as a technique for fracture toughness measurement (requiring only small samples of simple shape) and as an improved approach to prediction of ballistic impact outcomes.

Degree

thesis:*
Name dc:type.qualificationname
Doctor of Philosophy (PhD)
Level dc:type.qualificationlevel
Doctoral
Grantor dc:publisher.institution
University of Cambridge
Year dc:date.issued
2019

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Burley, Max
Advisor dc:contributor.advisor
  • Clyne, TW

Subjects

dc:subject × 7

Rights

dc:rights
Language dc:language
eng

Identifiers

dc:identifier.*
DOI dc:identifier.doi
https://doi.org/10.17863/CAM.53004
OAI identifier oai:identifier
oai:www.repository.cam.ac.uk:1810/305925

Chain of custody

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Harvested from
Cambridge University
Base URL
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Last updated
2026-07-22
Source record
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citation

Burley, Max. Extraction of mechanical properties over a range of strain rates from indentation data. Doctoral thesis, University of Cambridge, 2019. https://doi.org/10.17863/CAM.53004