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Quantitative evaluation of augmented strain at the weld metal during the Trans-Varestraint test
- Source :
- Welding in the World. 65:2013-2021
- Publication Year :
- 2021
- Publisher :
- Springer Science and Business Media LLC, 2021.
-
Abstract
- The hot cracking susceptibility in the Trans-Varestraint test was evaluated using the nominal strain calculated using the curvature radius of a bending block and the thickness of a specimen based on the theory of material mechanics. The nominal strain was calculated using the material properties at room temperature. Thus, in the Trans-Varestraint test, the non-uniformity of the strain around the weld part due to the temperature distribution is not considered. Therefore, the strain in the Trans-Varestraint test cannot be evaluated correctly. The aim of this study is to reveal the loaded strain at the weld metal to understand the evaluation of hot cracking susceptibility in the Trans-Varestraint test. The loaded strain around the trailing edge of the weld pool of pure iron was measured in-situ using a high-speed camera and high-resolution optical lens. The results of strains measured using image analysis and the finite-element method at the center of the weld bead were compared. Accordingly, it was clarified that the strain was concentrated on the weld part owing to the bending occurring along the weld line, and the strain exceeding the nominal strain was loaded to the trailing edge of the weld pool.
- Subjects :
- 0209 industrial biotechnology
Materials science
Strain (chemistry)
Mechanical Engineering
technology, industry, and agriculture
Metals and Alloys
Weld line
02 engineering and technology
Bending
Welding
respiratory system
020501 mining & metallurgy
law.invention
Cracking
020901 industrial engineering & automation
0205 materials engineering
Mechanics of Materials
law
Weld pool
Trailing edge
Composite material
Material properties
Subjects
Details
- ISSN :
- 18786669 and 00432288
- Volume :
- 65
- Database :
- OpenAIRE
- Journal :
- Welding in the World
- Accession number :
- edsair.doi...........62bc0ee3905f217c209fe16a0aa03bb2