Simulation of fatigue small crack growth in additive manufactured Ti–6Al–4V material
- Standort
-
Deutsche Nationalbibliothek Frankfurt am Main
- ISSN
-
1432-0959
- Umfang
-
Online-Ressource
- Sprache
-
Englisch
- Anmerkungen
-
online resource.
- Erschienen in
-
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
- Urheber
-
Gupta, A.
Sun, W.
Bennett, C. J.
- Beteiligte Personen und Organisationen
-
SpringerLink (Online service)
- DOI
-
10.1007/s00161-020-00878-0
- URN
-
urn:nbn:de:101:1-2020061619175940343561
- Rechteinformation
-
Open Access; Der Zugriff auf das Objekt ist unbeschränkt möglich.
- Letzte Aktualisierung
-
14.08.2025, 10:48 MESZ
Datenpartner
Dieses Objekt wird bereitgestellt von:
Deutsche Nationalbibliothek. Bei Fragen zum Objekt wenden Sie sich bitte an den Datenpartner.
Deutsche Nationalbibliothek. Bei Fragen zum Objekt wenden Sie sich bitte an den Datenpartner.
Beteiligte
- Gupta, A.
- Sun, W.
- Bennett, C. J.
- SpringerLink (Online service)
Ähnliche Objekte (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