Numerical and Experimental Investigation of Wrinkling Pattern for Aerospace Laminated Membrane Structures
Al-polymer laminated membranes are widely used in large aerospace structures. When the laminated membranes are pressurized, wrinkles emerge, which have an important effect on the performance of the structures during operation. This paper describes the numerical simulation and experimental investigat...
Saved in:
| Main Authors: | Yihong Hong, Wenjuan Yao, Yan Xu |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Wiley
2017-01-01
|
| Series: | International Journal of Aerospace Engineering |
| Online Access: | http://dx.doi.org/10.1155/2017/8476041 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Inversion analysis of constitutive relations of blade spar laminates with wrinkle defects
by: Ning Sun, et al.
Published: (2025-06-01) -
Numerical simulation study on the evolution of wrinkling defects in carbon fiber laminates based on spatial decomposition damage variable method
by: ZHENG Haocheng, et al.
Published: (2025-04-01) -
Investigation of Wrinkling Initiation in Shear Spinning
by: Li Zhikun, et al.
Published: (2025-01-01) -
Thermal nonreciprocity tuned by wrinkle patterns in graphene
by: Bohan Li, et al.
Published: (2024-01-01) -
Reactive substrate-driven interfacial polymerization for wrinkled polyamide membranes with enhanced permeance
by: Ping Xu, et al.
Published: (2025-06-01)