Experimental investigation on bending behavior of honeycomb sandwich panel with ceramic tile face-sheet

2019 ◽  
Vol 164 ◽  
pp. 280-286 ◽  
Author(s):  
Zhonggang Wang ◽  
Zhendong Li ◽  
Wei Xiong
Keyword(s):  
Experimental Investigation ◽  
Ceramic Tile ◽  
Sandwich Panel ◽  
Face Sheet ◽  
Honeycomb Sandwich ◽  
Bending Behavior

Numerical analysis of face sheet buckling for a CFRP/ Nomex honeycomb sandwich panel subjected to bending loading

2021 ◽  
pp. 114037
Author(s):  
Mae Oiwa ◽  
Toshio Ogasawara ◽  
Hajime Yoshinaga ◽  
Tsuyoshi Oguri ◽  
Takahira Aoki
Keyword(s):  
Numerical Analysis ◽  
Sandwich Panel ◽  
Face Sheet ◽  
Honeycomb Sandwich ◽  
Nomex Honeycomb ◽  
Bending Loading

scholarly journals Numerical Simulation of Projectile Oblique Impact on Microspacecraft Structure

2017 ◽  
Vol 2017 ◽  
pp. 1-9 ◽  
Author(s):  
Zhiyuan Zhang ◽  
Runqiang Chi ◽  
Baojun Pang ◽  
Gongshun Guan
Keyword(s):  
Sandwich Panel ◽  
Incident Angle ◽  
Hypervelocity Impact ◽  
Face Sheet ◽  
Front Face ◽  
Rear Face ◽  
Damage Area ◽  
Honeycomb Sandwich ◽  
Debris Cloud ◽  
Honeycomb Panel

In the present study, the microspacecraft bulkhead was reduced to the double honeycomb panel, and the projectile oblique hypervelocity impact on the double honeycomb panel was simulated. The distribution of the debris cloud and the damage of a honeycomb sandwich panel were investigated when the incident angles were set to be 60°, 45°, and 30°. The results showed that as incident angle decreased, the distribution of debris cloud was increased gradually, while the maximum perforation size of the rear face sheet was firstly increased with the decrease of the incident angle and then decreased. On the other hand, the damage area and the damage degree of the front face sheet of the second honeycomb panel layer were increased with the decrease of the incident angle. Finally, the critical angle of front and rear face sheets of the honeycomb sandwich panel was obtained under oblique hypervelocity impact.

Experimental investigation and design method on a lightweight bamboo-concrete sandwich panel under bending load

Structures ◽  
2021 ◽  
Vol 34 ◽  
pp. 856-874
Author(s):  
A. Basit F. Alla Fadlelmola ◽  
Zhihua Chen ◽  
Yansheng Du ◽  
Rui Ma ◽  
Jia Ma
Keyword(s):  
Experimental Investigation ◽  
Sandwich Panel ◽  
Design Method ◽  
Bending Load

Sound radiation and transmission loss characteristics of a honeycomb sandwich panel with composite facings: Effect of inherent material damping

2016 ◽  
Vol 383 ◽  
pp. 221-232 ◽  
Author(s):  
M.P. Arunkumar ◽  
M. Jagadeesh ◽  
Jeyaraj Pitchaimani ◽  
K.V. Gangadharan ◽  
M.C. Lenin Babu
Keyword(s):  
Sandwich Panel ◽  
Transmission Loss ◽  
Sound Radiation ◽  
Material Damping ◽  
Honeycomb Sandwich
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