ASTM-E399 2009
$58.50
E399-09e2 Standard Test Method for Linear-Elastic Plane-Strain Fracture Toughness Ic of Metallic Materials
Published By | Publication Date | Number of Pages |
ASTM | 2009 | 33 |
1.1 This test method covers the determination of fracture toughness ( K Ic ) of metallic materials under predominantly linear-elastic, plane-strain conditions using fatigue precracked specimens having a thickness of 1.6 mm (0.063 in.) or greater subjected to slowly, or in special (elective) cases rapidly, increasing crack-displacement force. Details of test apparatus, specimen configuration, and experimental procedure are given in the Annexes.
Note 1Plane-strain fracture toughness tests of thinner materials that are sufficiently brittle (see 7.1) can be made using other types of specimens (1) . There is no standard test method for such thin materials.
1.2 This test method is divided into two parts. The first part gives general recommendations and requirements for K Ic testing. The second part consists of Annexes that give specific information on displacement gage and loading fixture design, special 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.
PDF Catalog
PDF Pages | PDF Title |
---|---|
1 | Scope |
2 | Referenced Documents Terminology |
3 | FIG. 1 |
4 | Summary of Test Method Significance and Use |
5 | Apparatus FIG. 2 |
6 | Specimen Size, Configurations, and Preparation FIG. 3 FIG. 4 |
7 | FIG. 5 |
8 | General Procedure FIG. 6 |
9 | Calculation and Interpretation of Results |
10 | Report Precision and Bias FIG. 7 |
11 | FIG. 8 TABLE 1 |
12 | TABLE 2 TABLE 3 TABLE 4 |
13 | A1. DOUBLE-CANTILEVER DISPLACEMENT GAGE A1.1 FIG. A1.1 |
14 | A2. TESTING FIXTURES A2.1 Bend Specimen Loading Fixture A2.2 Compact Specimen Loading Clevis FIG. A1.2 |
15 | FIG. A2.1 |
16 | A3. SPECIAL REQUIREMENTS FOR TESTING BEND SPECIMENS A3.1 Specimen A3.2 Specimen Preparation A3.3 Apparatus FIG. A2.2 |
17 | A3.4 Procedure A3.5 Calculations |
18 | A4. SPECIAL REQUIREMENTS FOR TESTING COMPACT SPECIMENS A4.1 Specimen A4.2 Specimen Preparation A4.3 Apparatus A4.4 Procedure A4.5 Calculations FIG. A3.1 |
20 | A5. SPECIAL REQUIREMENTS FOR TESTING DISK-SHAPED COMPACT SPECIMENS A5.1 Specimen A5.2 Specimen Preparation A5.3 Apparatus A5.4 Procedure FIG. A4.1 |
21 | A5.5 Calculations FIG. A5.1 TABLE A5.1 |
22 | A6. SPECIAL REQUIREMENTS FOR TESTING ARC-SHAPED TENSION SPECIMENS A6.1 Specimen A6.2 Specimen Preparation A6.3 Apparatus |
23 | A6.4 Procedure FIG. A6.1 FIG. A6.2 |
24 | A6.5 Calculations |
25 | A7. SPECIAL REQUIREMENTS FOR TESTING ARC-SHAPED BEND SPECIMENS A7.1 Specimen A7.2 Specimen Preparation FIG. A7.1 |
26 | A7.3 Apparatus A7.4 Procedure FIG. A7.2 |
27 | A7.5 Calculations A8. FATIGUE PRECRACKING KIc FRACTURE TOUGHNESS SPECIMENS A8.1 Introduction A8.2 Equipment |
28 | A8.3 Specimen Requirements A8.4 Precracking Procedure |
29 | A9. SPECIAL REQUIREMENTS FOR TESTING HOT-PRESSED BERYLLIUM A9.1 Scope A9.2 Specimen Size, Configuration and Preparation A9.3 Testing and Record Analyses |
30 | A10. SPECIAL REQUIREMENTS FOR RAPID-FORCE, PLANE-STRAIN FRACTURE TOUGHNESS KIc (t) TESTING A10.1 Scope A10.2 Summary of Requirements A10.3 Significance and Use A10.4 Terminology A10.5 Apparatus A10.6 Procedure |
31 | A10.7 Calculation and Interpretation of Results FIG. A10.1 FIG. A10.2 |
32 | A10.8 Report A10.9 Precision and Bias REFERENCES |