Effect of fatigue loading on impact damage and buckling/post-buckling behaviors of stiffened composite panels under axial compression

2017 ◽  
Vol 164 ◽  
pp. 248-262 ◽  
Author(s):  
Yu Feng ◽  
Yuting He ◽  
Haoyu Zhang ◽  
Xiangfei Tan ◽  
Tao An ◽  
...  
Keyword(s):  
Axial Compression ◽  
Impact Damage ◽  
Fatigue Loading ◽  
Composite Panels ◽  
Stiffened Composite Panels ◽  
Post Buckling

Post-buckling reliability analysis of stiffened composite panels based on adaptive iterative sampling

2021 ◽  
Author(s):  
Feng Zhang ◽  
Mingying Wu ◽  
Xinting Hou ◽  
Cheng Han ◽  
Xinhe Wang ◽  
...  
Keyword(s):  
Reliability Analysis ◽  
Composite Panels ◽  
Stiffened Composite Panels ◽  
Iterative Sampling ◽  
Post Buckling

Impact damage detection of curved stiffened composite panels by using wavy embedded small-diameter optical fibers

2002 ◽  
Author(s):  
Hiroaki Tsutsui ◽  
Akio Kawamata ◽  
Junichi Kimoto ◽  
Tomio Sanda ◽  
Nobuo Takeda
Keyword(s):  
Damage Detection ◽  
Optical Fibers ◽  
Impact Damage ◽  
Small Diameter ◽  
Composite Panels ◽  
Stiffened Composite Panels

Post-buckling behaviour of flat stiffened composite panels: Experiments vs. analysis

2012 ◽  
Vol 94 (12) ◽  
pp. 3421-3433 ◽  
Author(s):  
L. Boni ◽  
D. Fanteria ◽  
A. Lanciotti
Keyword(s):  
Composite Panels ◽  
Stiffened Composite Panels ◽  
Post Buckling

scholarly journals Prediction of the Compresion-After-Impact Strength of Thin-Skin Stiffened Composite Panels

2000 ◽  
Vol 9 (4) ◽  
pp. 096369350000900 ◽  
Author(s):  
Y. Zhuk ◽  
C. Soutis ◽  
I. Guz
Keyword(s):  
Impact Damage ◽  
Low Velocity Impact ◽  
Composite Panels ◽  
Low Velocity ◽  
Damage Initiation ◽  
Mechanics Model ◽  
Stiffened Composite Panels ◽  
Open Hole ◽  
Thin Skin ◽  
The Impact

The compressive response of thin-skin stiffened composite panels with low velocity impact damage is examined. The finite element method together with the Soutis-Fleck fracture mechanics model is used to predict damage initiation in the form of fibre microbuckling in the 0° plies, propagation and final failure; in the model the impact damage is replaced with an equivalent circular or elliptical open hole. Theoretical results are compared to experimental data and found in good agreement.

Postbuckling and failure of stiffened composite panels under axial compression

1998 ◽  
Vol 42 (1) ◽  
pp. 13-21 ◽  
Author(s):  
Cheol-Won Kong ◽  
In-Cheol Lee ◽  
Chun-Gon Kim ◽  
Chang-Sun Hong
Keyword(s):  
Axial Compression ◽  
Composite Panels ◽  
Stiffened Composite Panels
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