Validation of modeling the delamination process of composite panels of load-bearing elements of aircraft structures
Both in the manufacture and operation of structural elements made of layered composite materials, interlayer defects may occur upon impact as a result of operation or violation of manufacturing technology, which significantly reduces the strength characteristics of such structures. Therefore, taking...
Saved in:
| Main Author: | I. S. Belousov |
|---|---|
| Format: | Article |
| Language: | Russian |
| Published: |
Association «Technology Platform «National Information Satellite System»
2024-01-01
|
| Series: | Космические аппараты и технологии |
| Subjects: | |
| Online Access: | http://journal-niss.ru/journal/archive/50/paper1.pdf |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Extreme performance of multi-layer laminated glass designs under blast loads
by: Andrew Bowman, et al.
Published: (2025-07-01) -
Structural behavior of window laminated glass plies using new interlayer materials
by: Mostafa El-Shami, et al.
Published: (2018-01-01) -
Influence of effective thickness in elastic anisotropy and surface acoustic wave propagation in CoFeB/Au multilayer
by: A. V. Achuthan, et al.
Published: (2025-07-01) -
Study on the ultimate bearing capacity of high steel grade elbow with trench defects
by: ZHANG Tao, et al.
Published: (2025-06-01) -
Interfacial delamination on fan-out wafer-level package using finite element analysis
by: Ariel P. Conversion, et al.
Published: (2025-06-01)