ASTM International - ASTM E1304-97(2014)

Standard Test Method for Plane-Strain (Chevron-Notch) Fracture Toughness of Metallic Materials

inactive

Organization:	ASTM International
Publication Date:	1 July 2014
Status:	inactive
Page Count:	12
ICS Code (Mechanical testing of metals):	77.040.10

significance And Use:

5.1 The fracture toughness determined by this test method characterizes the resistance of a material to fracture by a slowly advancing steady-state crack (see 3.2.5) in a neutral environment under severe tensile constraint. The state of stress near the crack front approaches plane strain, and the crack-tip plastic region is small compared with the crack size and specimen dimensions in the constraint direction. A K_Iv or K_Ivj value may be used to estimate the relation between failure stress and defect size when the conditions described above would be expected, although the relationship may differ from that obtained from a K_Ic value (see Note 1). Background information concerning the basis for development of this test method in terms of linear elastic fracture mechanics may be found in Refs (6-15).

5.1.1 The K_Iv, K_Ivj, or K_IvM value of a given material can be a function of testing speed (strain rate) and temperature. Furthermore, cyclic forces can cause crack extension at K_I values less than K_Iv, and crack extension can be increased by the presence of an aggressive environment. Therefore, application of K_Iv in the design of service components should be made with an awareness of differences that may exist between the laboratory tests and field conditions.

5.1.2 Plane-strain fracture toughness testing is unusual in that there can be no advance assurance that a valid K_Iv, K_Ivj, or K_IvM will be determined in a particular test. Therefore, it is essential that all the criteria concerning the validity of results be carefully considered as described herein.

5.2 This test method can serve the following purposes:

5.2.1 To establish the effects of metallurgical variables such as composition or heat treatment, or of fabricating operations such as welding or forming, on the fracture toughness of new or existing materials.

5.2.2 For specifications of acceptance and manufacturing quality control, but only when there is a sound basis for specification of minimum K_Iv, K_Ivj, or K_IvM values, and then only if the dimensions of the product are sufficient to provide specimens of the size required for valid K_Iv determination (9). The specification of K_Iv values in relation to a particular application should signify that a fracture control study has been conducted on the component in relation to the expected history of loading and environment, and in relation to the sensitivity and reliability of the crack detection procedures that are to be applied prior to service and subsequently during the anticipated life.

5.2.3 To provide high spatial resolution in measuring plane strain fracture toughness variations in parent pieces of material (14).

Note 2: The high spatial resolution is possible because of the small allowable specimen size criterion, B ≥1.25 (K_Iv/σ_YS)² (9), and because the toughness is measured at approximately the midline of the specimen, and only in the material covered by the crack's lateral extent, which is about one third of the specimen's lateral dimension, B.

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scope:

1.1 This test method covers the determination of plane-strain (chevron-notch) fracture toughnesses, K_Iv or K_IvM, of metallic materials. Fracture toughness by this method is relative to a slowly advancing steady state crack initiated at a chevron-shaped notch, and propagating in a chevron-shaped ligament (Fig. 1). Some metallic materials, when tested by this method, exhibit a sporadic crack growth in which the crack front remains nearly stationary until a critical load is reached. The crack then becomes unstable and suddenly advances at high speed to the next arrest point. For these materials, this test method covers the determination of the plane-strain fracture toughness, K_Ivj or K_IvM, relative to the crack at the points of instability.

(A) See Fig. 6. (A) See Fig. 6.(B) See Note 1. (A) Compiled from Refs (1), (2), (3), and (4), and using the polynomials in Table 5.(B) Minimum value of Y*. (A) Compiled from Refs (1), (2), (3), and (4).(B) Y* = exp[C₀ + C₁r + C₂r² + C₃r³ + C₄r⁴], accuracy ±0.5 %.(C) Estimated from finite element analysis (3), and extrapolated equation from Ref (4). Accuracy for 0.3 ≤ r ≤ 0.85 is ±0.5 %.(D) Extrapolated from equations in Ref (4). Accuracy estimated to be ±0.5 % for 0.2 ≤ r ≤ 0.85.(E) Equation from Ref (4). Accuracy estimated to be± 0.5 % for 0.15 ≤ r ≤ 0.6.