BS ISO 15850:2014
$142.49
Plastics. Determination of tension-tension fatigue crack propagation. Linear elastic fracture mechanics (LEFM) approach
Published By | Publication Date | Number of Pages |
BSI | 2014 | 32 |
This International Standard specifies a method for measuring the propagation of a crack in a notched specimen subjected to a cyclic tensile load varying between a constant positive minimum and a constant positive maximum value. The test results include the crack length as a function of the number of load cycles and the crack length increase rate as a function of the stress intensity factor and energy release rate at the crack tip. The possible occurrence of discontinuities in crack propagation is detected and reported.
The test can be also used for the purpose of determining the resistance to crack propagation failure. In this case, the results can be presented in the form of number of cycles to failure or total time taken to cause crack propagation failure versus the stress intensity factor (see Annex A).
The method is suitable for use with the following range of materials:
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rigid and semi-rigid thermoplastic moulding and extrusion materials (including filled and short-fibre-reinforced compounds) plus rigid and semi-rigid thermoplastic sheets;
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rigid and semi-rigid thermosetting materials (including filled and short-fibre-reinforced compounds) plus rigid and semi-rigid thermosetting sheets.
PDF Catalog
PDF Pages | PDF Title |
---|---|
6 | Foreword |
7 | Section sec_1 Section sec_2 Section sec_3 Section sec_3.1 Section sec_3.2 1 Scope 2 Normative references 3 Terms and definitions |
8 | Section sec_3.3 Section sec_3.4 Section sec_3.5 Section sec_3.6 Section sec_3.7 Section sec_3.8 Section sec_3.9 |
9 | Section sec_3.10 Section sec_3.11 Section sec_3.12 Section sec_3.13 Section sec_3.14 Section sec_3.15 |
10 | Section sec_3.16 Section sec_3.17 Section sec_3.18 Section sec_3.19 Section sec_3.20 Section sec_3.21 Section sec_3.22 Section sec_3.23 |
11 | Section sec_4 Section sec_5 4 Principle 5 Significance and use |
12 | Section sec_6 Section sec_6.1 Section sec_6.1.1 Section sec_6.1.2 6 Test specimens 6.1 Shape and size |
13 | Table tab_b Figure fig_1 |
14 | Table tab_c Figure fig_2 Section sec_6.1.3 |
15 | Figure fig_3 Section sec_6.2 Section sec_6.3 6.2 Preparation 6.3 Notching |
16 | Section sec_6.4 Section sec_6.5 Section sec_7 Section sec_7.1 Section sec_7.1.1 Section sec_7.1.2 6.4 Side grooves 6.5 Conditioning 7 Apparatus 7.1 Test machine |
17 | Section sec_7.1.3 Section sec_7.1.4 Section sec_7.2 Section sec_7.3 Section sec_7.3.1 7.2 Grips 7.3 Crack length measurement |
18 | Section sec_7.3.2 Section sec_7.3.3 Section sec_7.3.4 |
19 | Table tab_f Figure fig_4 |
20 | Table tab_1 Section sec_7.3.5 |
21 | Section sec_7.4 Section sec_8 Section sec_8.1 Section sec_8.2 Section sec_8.3 Section sec_8.4 Section sec_8.5 Section sec_8.6 7.4 Test atmosphere 8 Test procedure 8.1 Measurement of specimen dimensions 8.2 Specimen mounting 8.3 Loading 8.4 Out-of-plane crack propagation 8.5 Discontinuous crack propagation 8.6 Number of tests |
22 | Section sec_9 Section sec_9.1 Section sec_9.2 Section sec_9.3 Section sec_9.4 9 Calculation and interpretation of results 9.1 Crack length versus number of cycles 9.2 Crack curvature correction 9.3 Crack growth rate da/dN 9.4 Stress intensity factor range ΔK |
23 | Section sec_9.5 Section sec_10 Section sec_10.1 Section sec_10.2 9.5 Energy release rate range ΔG 10 Test report 10.1 General 10.2 For fatigue crack propagation test |
24 | Section sec_10.3 10.3 For fatigue crack propagation to failure test |
25 | Annex sec_A Annex A (informative) Abnormality in the use of cyclic fatigue crack propagation test for ranking long-term static fatigue behaviour |
26 | Table tab_g Figure fig_A.1 |
27 | Table tab_h Figure fig_A.2 |
28 | Table tab_i Figure fig_A.3 |
29 | Reference ref_1 Reference ref_2 Reference ref_3 Reference ref_4 Reference ref_5 Reference ref_6 Reference ref_7 Reference ref_8 Reference ref_9 Reference ref_10 Bibliography |