Cargando…
Experimental Study on Vibration Fatigue Behavior of Aircraft Aluminum Alloy 7050
It has been previously noted that the development of aerospace material technology and breakthroughs are inseparable when obtaining great achievements in the aerospace industry. Materials are the basis and precursor of modern high technology and industry. As one of the most powerful aluminium alloys...
Autores principales: | Teng, Yunnan, Xie, Liyang, Zhang, Hongyuan |
---|---|
Formato: | Online Artículo Texto |
Lenguaje: | English |
Publicado: |
MDPI
2022
|
Materias: | |
Acceso en línea: | https://www.ncbi.nlm.nih.gov/pmc/articles/PMC9658166/ https://www.ncbi.nlm.nih.gov/pubmed/36363147 http://dx.doi.org/10.3390/ma15217555 |
Ejemplares similares
-
A Study on the Susceptibility to SCC of 7050 Aluminum Alloy by DCB Specimens
por: Qi, Xing, et al.
Publicado: (2016) -
Fatigue Characteristics of 7050-T7451 Aluminum Alloy Friction Stir Welding Joints and the Stress Ratio Effect
por: Zhu, Hanji, et al.
Publicado: (2022) -
Microstructure Evolution of the Near-Surface Deformed Layer and Corrosion Behavior of Hot Rolled AA7050 Aluminum Alloy
por: Liu, Ergen, et al.
Publicado: (2023) -
Effect of Cold Pressing Deformation on Microstructure and Residual Stress of 7050 Aluminum Alloy Die Forgings
por: Li, Huiqu, et al.
Publicado: (2023) -
Microstructural Evolution and Hardness Responses of 7050 Al Alloy during Processing
por: Zhou, Yuting, et al.
Publicado: (2022)