BS ISO 12108:2002:2003 Edition
$189.07
Metallic materials. Fatigue testing. Fatigue crack growth method
Published By | Publication Date | Number of Pages |
BSI | 2003 | 48 |
PDF Catalog
PDF Pages | PDF Title |
---|---|
3 | TitlePage – Metallic materials�— Fatigue testing�— Fatigue crack growth method |
5 | TableofContent – Contents Page |
6 | Foreword – Foreword |
7 | Introduction – Introduction |
9 | Scope – 1��� Scope NormativeReference – 2��� Normative reference |
11 | Clause1 – 4��� Symbols and abbreviations Subclause2 – 4.1��� Symbols |
12 | Subclause2 – 4.2��� Abbreviations for specimen identification Clause1 – 5��� Apparatus Subclause2 – 5.1��� Testing machine Subclause3 – 5.1.1��� General |
13 | Subclause3 – 5.1.2��� Testing machine alignment Subclause3 – 5.1.3��� Force measuring system Subclause2 – 5.2��� Cycle-counter Subclause2 – 5.3��� Grips and fixtures for CT specimens |
14 | Subclause2 – 5.4��� Grips and fixtures for CCT/SENT specimens Subclause3 – 5.4.1��� General |
15 | Subclause3 – 5.4.2��� Tension-tension testing of a CCT specimen |
16 | Subclause3 – 5.4.3��� Tension-compression testing of a CCT specimen |
17 | Subclause3 – 5.4.4��� Alignment of CCT specimen grips |
18 | Subclause2 – 5.5��� Grips and fixtures for the SENB specimens Subclause3 – 5.5.1��� Tension-compression grips for the SENB8 specimen |
19 | Subclause3 – 5.5.2��� Tension-tension testing of SENB specimens |
20 | Subclause2 – 5.6��� Crack length measurement apparatus Subclause3 – 5.6.1��� General Subclause3 – 5.6.2��� Non-visual crack length measurement Subclause3 – 5.6.3��� Visual crack length measurement Clause1 – 6��� Specimens Subclause2 – 6.1��� General |
24 | Subclause2 – 6.2��� Crack plane orientation |
25 | Subclause2 – 6.3��� Starter notch precracking details |
26 | Subclause2 – 6.4��� Stress intensity factor Subclause3 – 6.4.1��� General |
27 | Subclause3 – 6.4.2��� Compact tension, CT, specimen Subclause3 – 6.4.3��� Centre cracked tension, CCT, specimen Subclause3 – 6.4.4��� Single edge notch three point bend, SENB3, specimen Subclause3 – 6.4.5��� Single edge notch four point bend, SENB4, specimen |
28 | Subclause3 – 6.4.6��� Single edge notch eight point bend, SENB8, specimen Subclause3 – 6.4.7��� Single edge notch tension, SENT, specimen Subclause2 – 6.5��� Specimen size Subclause3 – 6.5.1��� General |
29 | Subclause3 – 6.5.2��� CT specimen minimum uncracked ligament Subclause3 – 6.5.3��� CCT specimen minimum uncracked ligament Subclause3 – 6.5.4��� SENB specimen minimum uncracked ligament Subclause3 – 6.5.5��� SENT specimen minimum uncracked ligament Subclause2 – 6.6��� Specimen thickness Subclause3 – 6.6.1��� General Subclause3 – 6.6.2��� CT specimen |
30 | Subclause3 – 6.6.3��� CCT specimen Subclause3 – 6.6.4��� SENB specimen Subclause3 – 6.6.5��� SENT specimen Subclause2 – 6.7��� Residual stresses Clause1 – 7��� Procedure Subclause2 – 7.1��� Fatigue precracking |
31 | Subclause2 – 7.2��� Crack length measurement Subclause2 – 7.3��� Constant-force-amplitude, |
32 | Subclause2 – |
34 | Clause1 – 8��� Crack length measurement Subclause2 – 8.1��� Resolution Subclause2 – 8.2��� Interruption Subclause2 – 8.3��� Static force Subclause2 – 8.4��� Measurement interval |
35 | Subclause2 – 8.5��� Symmetry Subclause2 – 8.6��� Out-of-plane cracking Subclause2 – 8.7��� Crack tip bifurcation Clause1 – 9��� Calculations Subclause2 – 9.1��� Crack front curvature Subclause2 – 9.2��� Determining the fatigue crack growth rate Subclause3 – 9.2.1��� General |
36 | Subclause3 – 9.2.2��� Secant method Subclause3 – 9.2.3��� Incremental polynomial method Subclause2 – 9.3��� Determination of the fatigue crack growth threshold Clause1 – 10��� Test report Subclause2 – 10.1��� General |
37 | Subclause2 – 10.2��� Material Subclause2 – 10.3��� Test specimen Subclause2 – 10.4��� Precracking terminal values Subclause2 – 10.5��� Test conditions |
38 | Subclause2 – 10.6��� Test analysis Subclause2 – 10.7��� Presentation of results |
45 | Bibliography – Bibliography |