STIFFENER-SKIN INTERFACE FAILURE CHARACTERIZATION OF THE STIFFENED COMPOSITE PANEL AT POST-BUCKLING STAGE
A six-point bending test that characterized the failure of the stiffener-skin interface of a stiffened composite panel at the post-buckling stage is studied. A FEM model for a stiffened panel subjected to compression and a six-point bending test model were created in Abaqus. The initial failure loca...
Saved in:
Main Authors: | HU BoTao, CHAI YaNan, CHEN XiangMing, WEI JingChao |
---|---|
Format: | Article |
Language: | zho |
Published: |
Editorial Office of Journal of Mechanical Strength
2019-01-01
|
Series: | Jixie qiangdu |
Subjects: | |
Online Access: | http://www.jxqd.net.cn/thesisDetails#10.16579/j.issn.1001.9669.2019.06.031 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
The Effects of Ply Orientation on Nonlinear Buckling of Aircraft composite Stiffened Panel
by: Ouadia Mouhat, et al.
Published: (2019-08-01) -
Effects of ply orientation on nonlinear buckling of Aircraft composite stiffened panel
by: Ouadia Mouhat, et al.
Published: (2019-10-01) -
ANALYSIS OF THE INFLUENCE OF STIFFENER TYPE AND MANUFACTURING PROCESS ON MECHANICAL BEHAVIOR OF TITANIUM ALLOY STIFFENED PANEL UNDER AXIAL COMPRESSION
by: WANG ZhaoHui, et al.
Published: (2022-01-01) -
STUDY THE EFFECT OF SHOT PEENING RESIDUAL STRESSES ON COMPRESSIVE STRENGTH OF STIFFENED PANEL
by: ZHANG ZiPeng, et al.
Published: (2020-01-01) -
APPLICABILITY INVESTIGATION OF FAILURE CRITERION FOR POST-BUCKLING ANALYSIS OF STIFFENED COMPOSITE PANELS
by: LIN GuoWei, et al.
Published: (2020-01-01)