Cold Expansion Strengthening of 7050 Aluminum Alloy Hole: Structure, Residual Stress, and Fatigue Life
The 7050 aluminum alloy orifice plate is extruded and strengthened by the cold expansion process of slotted bushing holes. A three-dimensional finite element model was established for cold expansion strengthening of holes, and the residual stress distribution of 7050 aluminum alloy orifice plates is...
Saved in:
| Main Authors: | Qi Li, Qichao Xue, Quansheng Hu, Ting Song, Yonghui Wang, Siyang Li |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Wiley
2022-01-01
|
| Series: | International Journal of Aerospace Engineering |
| Online Access: | http://dx.doi.org/10.1155/2022/4057898 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Research on residual stress and deformation control of domestic 7050 aluminum alloy thin-wall bearing frame turning
by: HU Yue, et al.
Published: (2025-04-01) -
Creep constitutive model of 7050⁃T7451 aluminum alloy based on damage mechanics
by: LI Jie, et al.
Published: (2025-05-01) -
Influence of Grain Boundary on the Fatigue Crack Growth of 7050-T7451 Aluminum Alloy Based on Small Time Scale Method
by: Weihan Wang, et al.
Published: (2016-01-01) -
Microstructure and Properties of 7050-T74 Aluminum Alloys with Different Zn/Mg Ratios
by: Daihong Xiao, et al.
Published: (2024-10-01) -
Study on hydrogen-assisted stress corrosion cracking behavior of 7050 aluminum alloy
by: Qiang Zhang, et al.
Published: (2025-03-01)