Simulation of fatigue small crack growth in additive manufactured Ti–6Al–4V material
- Location
-
Deutsche Nationalbibliothek Frankfurt am Main
- ISSN
-
1432-0959
- Extent
-
Online-Ressource
- Language
-
Englisch
- Notes
-
online resource.
- Bibliographic citation
-
Simulation of fatigue small crack growth in additive manufactured Ti–6Al–4V material ; day:25 ; month:3 ; year:2020 ; pages:1-17
Continuum mechanics and thermodynamics ; (25.3.2020), 1-17
- Creator
-
Gupta, A.
Sun, W.
Bennett, C. J.
- Contributor
-
SpringerLink (Online service)
- DOI
-
10.1007/s00161-020-00878-0
- URN
-
urn:nbn:de:101:1-2020061619175940343561
- Rights
-
Open Access; Der Zugriff auf das Objekt ist unbeschränkt möglich.
- Last update
-
14.08.2025, 10:48 AM CEST
Data provider
This object is provided by:
Deutsche Nationalbibliothek. If you have any questions about the object, please contact the data provider.
Deutsche Nationalbibliothek. If you have any questions about the object, please contact the data provider.
Associated
- Gupta, A.
- Sun, W.
- Bennett, C. J.
- SpringerLink (Online service)
Other Objects (12)
High Temperature Fatigue Crack Growth Behavior of Ti-6Al-4V
Fatigue Crack Segmentation and Characterization of Additively Manufactured Ti‐6Al‐4V Using X‐Ray Computed Tomography
Characterization of the hot forming behavior of additively manufactured Ti-6Al-4V
Factors affecting the fatigue strength of additively manufactured Ti-6Al-4V parts
Fatigue Property of Additively Manufactured Ti-6Al-4V under Nonproportional Multiaxial Loading
Effects of defects in laser additive manufactured Ti-6Al-4V on fatigue properties
Crystallography of Fatigue Crack Initiation and Growth in Fully Lamellar Ti-6Al-4V
Process Chain Design for Post-Processing of Wire and Arc Additively Manufactured Ti-6Al-4V
Comparative Study of Room and Cryogenic Deformation Behavior of Additive Manufactured Ti–6Al–4V Alloy
High cycle fatigue and fatigue crack propagation behaviors of β-annealed Ti-6Al-4V alloy
Ressourceneffiziente Zerspanung von Ti-6Al-4V-Strukturbauteilen für Luftfahrtanwendungen
Einfluss chemischer Oberflächennachbehandlungen auf additiv gefertigtes Ti-6Al-4V
High Temperature Fatigue Crack Growth Behavior of Ti-6Al-4V
Fatigue Crack Segmentation and Characterization of Additively Manufactured Ti‐6Al‐4V Using X‐Ray Computed Tomography
Characterization of the hot forming behavior of additively manufactured Ti-6Al-4V
Factors affecting the fatigue strength of additively manufactured Ti-6Al-4V parts
Fatigue Property of Additively Manufactured Ti-6Al-4V under Nonproportional Multiaxial Loading
Effects of defects in laser additive manufactured Ti-6Al-4V on fatigue properties
Crystallography of Fatigue Crack Initiation and Growth in Fully Lamellar Ti-6Al-4V
Process Chain Design for Post-Processing of Wire and Arc Additively Manufactured Ti-6Al-4V
Comparative Study of Room and Cryogenic Deformation Behavior of Additive Manufactured Ti–6Al–4V Alloy
High cycle fatigue and fatigue crack propagation behaviors of β-annealed Ti-6Al-4V alloy
Ressourceneffiziente Zerspanung von Ti-6Al-4V-Strukturbauteilen für Luftfahrtanwendungen
Einfluss chemischer Oberflächennachbehandlungen auf additiv gefertigtes Ti-6Al-4V
High Temperature Fatigue Crack Growth Behavior of Ti-6Al-4V
Fatigue Crack Segmentation and Characterization of Additively Manufactured Ti‐6Al‐4V Using X‐Ray Computed Tomography
Characterization of the hot forming behavior of additively manufactured Ti-6Al-4V
Factors affecting the fatigue strength of additively manufactured Ti-6Al-4V parts
Fatigue Property of Additively Manufactured Ti-6Al-4V under Nonproportional Multiaxial Loading
Effects of defects in laser additive manufactured Ti-6Al-4V on fatigue properties
Crystallography of Fatigue Crack Initiation and Growth in Fully Lamellar Ti-6Al-4V
Process Chain Design for Post-Processing of Wire and Arc Additively Manufactured Ti-6Al-4V
Comparative Study of Room and Cryogenic Deformation Behavior of Additive Manufactured Ti–6Al–4V Alloy
High cycle fatigue and fatigue crack propagation behaviors of β-annealed Ti-6Al-4V alloy
Ressourceneffiziente Zerspanung von Ti-6Al-4V-Strukturbauteilen für Luftfahrtanwendungen