PREN 3873 : 200P1
Withdrawn
AEROSPACE SERIES - TEST METHODS FOR METALLIC MATERIALS - DETERMINATION OF FATIGUE CRACK GROWTH RATES USING CORNER-CRACKED (CC) TEST PIECES
Hardcopy , PDF
English
07-23-2013
Foreword
Introduction
1 Scope
2 Normative references
3 Symbols and abbreviations
4 General
5 Resources
6 Test pieces
7 Procedures
8 Health and Safety
9 Evaluation of results
10 Test record
Annex A (normative) - Information on measuring crack depths
in corner-crack test pieces with the direct-current
- Potential-drop method
Annex B (normative) - Stress-intensity function for corner-crack
test pieces
Annex C (normative) - Guidelines on test piece handling and
degreasing
Describes the requirements for determining fatigue crack growth rates using the corner-crack (CC) test piece. Crack development is measured using a potential-drop system, and the calculated crack depths can be corrected via marker bands created on the fracture surface during the test.
| DocumentType |
Draft
|
| Pages |
31
|
| PublisherName |
Aerospace & Defence Industries Association of Europe
|
| Status |
Withdrawn
|
| Standards | Relationship |
| NF EN 3873 : 2012 | Identical |
| 01/705746 DC : 0 | Identical |
| PREN 4800-001 : 200P2 | AEROSPACE SERIES - TITANIUM AND TITANIUM ALLOYS - TECHNICAL SPECIFICATION - PART 1: PLATE, SHEET AND STRIP |
| BS EN 4800-001:2010 | Aerospace series. Titanium and titanium alloys. Technical specification Plate, sheet and strip |
| EN ISO 3785:2006 | Metallic materials - Designation of test specimen axes in relation to product texture (ISO 3785:2006) |
| EN 2002-002:2005 | Aerospace series - Metallic materials - Test methods - Part 2: Tensile testing at elevated temperature |
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