Apr + Designation: E – 90 (Reapproved ). Standard Test Method for This test method is under the jurisdiction of ASTM Committee E-8 on. Futgue and . Properties and Testing of Materialsداوملا رابتخاو صاوخ ميحرلا نمحرلا لا مسب Determination of Fracture Toughness “Plane-S. This standard is issued under the fixed designation E ; the number immediately following the designation indicates the 1 This test method is under the jurisdiction of ASTM Committee E08 on Fatigue .. Note 2—Cutter tip angle 90° max.
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Specimen Size, Configurations, and Preparation see also 1. Fatigue Precracking KIc Specimens. Historical Version s – view previous versions of standard. Likewise this test method does not apply to high toughness or e399-09 tearing-resistance materials whose failure is accompanied by appreciable amounts of plasticity.
Active view current version of standard. General information and requirements common to all specimen types are listed as follows: Bend Specimen SE B.
ASTM E Standard Test Method for Plane-Strain Fracture – Google Books
It is the e399-9 of the user of this standard to establish appro- priate safety and health practices and determine the applica- bility of regulatory limitations prior to use. In addition, an annex is provided for the specific procedures to be followed in asm plane-strain fracture toughness tests.
This standard has been approved for use by agencies of the Department of Defense. Enviado por Giulio flag Denunciar. Crack extension under cyclic or sustained forces as by stress corrosion cracking or creep crack growth can be influenced by temperature and environment.
In addition, an annex is provided for the specific procedures to be followed in d399-90 plane-strain fracture toughness tests. The effect can be especially significant for specimens removed from as-heat treated or otherwise non-stress relieved stock, from weldments, from complex wrought parts, or from parts with intentionally induced residual stresses.
E — 90 Reapproved Standard Test Method for Plane-Strain Fracture Toughness of Metallic Materials1 This standard is issued under the fixed designation E ; the number immediately following the designation indicates the year of e399-0 adoption or, in the case of revision, the year of last revision.
The orientation of the crack plane should be identified wherever possible in accordance with the following systems Specimen Size Validity Requirements. Apparatus see also 1. There is no standard test method for testing such thin materials. The first part gives general recommendations and requirements for K Ic testing. The first part gives general information concerning the recommendations and requirements for Ic testing.
Crack Extension Beyond Starter Notch. A superscript epsilon e indicates an editorial e99-90 since the last revision or reapproval. Note 1-Plane-strain fracture toughness tests of thinner materials that are sufficiently brittle see 7. The second part consists of Annexes that asstm specific information on displacement gage and loading fixture design, e399-990 requirements for individual specimen configurations, and detailed procedures for fatigue precracking.
Additional annexes are provided that give specific procedures for beryllium and rapid-force testing. The details of the various specimen and test configurations are shown in Annexes A1 through A7 and A9.
w399-90 The specification of K Ic values in relation to a particular application should signify that a fracture control study has been conducted for the component in relation to the expected loading and environment, and in relation to the sensitivity and reliability of the crack detection procedures that asgm to be applied prior to service and subsequently during the anticipated life.
General information and requirements common to all specimen types are listed as follows:.
Therefore, when K Ic is applied to the design of service components, differences between laboratory test and field conditions shall be considered. NOTE 1—Plane-strain fracture toughness tests of thinner materials that are sufficiently brittle see 7.
Background information concerning the basis for development of this test method in terms of linear elastic fracture mechanics may be found in Refs 1 and 2. Originally published as E — 70 T. Compact Specimen Loading Clevis. General information and requirements common to all specimen types are listed as follows: This strength ratio is a function of the maximum load the specimen can sustain, its initial dimensions and the yield strength of the material.
ASTM E399 (Standard Test Method for Plane Strain Fracture Toughness for Metallic Materials)
Work Item s – proposed revisions of this standard. Work Item s – proposed revisions of this standard. Bend Specimen Loading Fixture. Guidance on testing elastic-plastic materials is given in Test Method E Therefore, compliance with the specified validity criteria of this test method is essential. The present test method does not apply to such materials and the user is referred to Test Method E and E Link to Active This link will always route to the current Active version of the standard.
It is the responsibility of the user of this standard to establish appropriate safety and health practices and determine the applicability of regulatory limitations prior to use. Standard and Alternative Specimen Configurations. Details of test apparatus, specimen configuration, and experimental procedure are given in the Annexes.
It is the responsibility of the user of this standard to establish appropriate safety, health, and environmental practices and determine the applicability of regulatory limitations prior to use.
The first part gives general information concerning the recommenda- tions and requirements for KIc testing. Compact Specimen C T.
In addition, the product form should be identified for example, straight-rolled plate, cross-rolled plate, pancake forging, etc.