A protocol for characterizing the structural performance of metallic sandwich panels: application to pyramidal truss cores

2004 ◽  
Vol 41 (22-23) ◽  
pp. 6249-6271 ◽  
Author(s):  
F.W. Zok ◽  
S.A. Waltner ◽  
Z. Wei ◽  
H.J. Rathbun ◽  
R.M. McMeeking ◽  
...  
2018 ◽  
Vol 25 (4) ◽  
pp. 797-805 ◽  
Author(s):  
R.S. Jayaram ◽  
V.A. Nagarajan ◽  
K.P. Vinod Kumar

Abstract Honeycomb sandwich panels entice continuously enhanced attention due to its excellent mechanical properties and multi-functional applications. However, the principal problem of sandwich panels is failure by face/core debond. Novel lightweight sandwich panels with hybrid core made of honeycomb, foam and through-thickness pin was developed. Reinforcing polyester pins between faces and core is an effectual way to strengthen the core and enhance the interfacial strength between the face/core to improve the structural performance of sandwich panels. To provide feasibility for pin reinforcement, honeycomb core was pre-filled with foam. Mechanical properties enhancement due to polyester pinning were investigated experimentally under flatwise compression, edgewise compression and flexural test. The experimental investigations were carried out for both “foam filled honeycomb sandwich panels” (FHS) and “polyester pin-reinforced foam filled honeycomb sandwich panels” (PFHS). The results show that polyester pin reinforcement in foam filled honeycomb sandwich panel enhanced the flatwise, edgewise compression and flexural properties considerably. Moreover, increasing the pin diameter has a larger effect on the flexural rigidity of PFHS panels. PFHS panels have inconsequential increase in weight but appreciably improved their structural performance.


Author(s):  
F. W. Zok * ◽  
H. Rathbun ◽  
M. He ◽  
E. Ferri ◽  
C. Mercer ◽  
...  

Proceedings ◽  
2018 ◽  
Vol 2 (15) ◽  
pp. 1152
Author(s):  
Aidan Reilly ◽  
Richard O'Hegarty ◽  
Oliver Kinnane

This paper presents work developing thin precast concrete sandwich panels for recladding and overcladding applications. These panels are designed for the retrofit of precast concrete structures where the underlying frame is structurally sound. Structural and thermal testing has been carried out to validate the performance of the panels. The panels are designed to have thermal performance better than current national standards, and this has been verified through hot-box testing of components and small-scale panels. Structural performance of the panels has been tested with 3 point bending tests on full-scale panels. Work is in progress towards demonstration of the panels on an occupied building in the UK.


2018 ◽  
Vol 22 (6) ◽  
pp. 1859-1878 ◽  
Author(s):  
Shanshan Shi ◽  
Bingzhi Chen ◽  
Zhi Sun

Combining the complementary properties of honeycomb cores and grid cores, a composite sandwich panel with honeycomb–grid hybrid core was proposed to enhance the structural performance of composite sandwich panels. However, important gaps remain in calculating the structural performance of the composite sandwich panels. In this paper, an equivalent stiffness model was proposed to analytically estimate the stiffness matrix of composite sandwich panels with honeycomb–grid hybrid core. The reliability and accuracy of the equivalent stiffness model were verified by experimental measurements from three-point bending tests. Furthermore, the effects of face-sheet thickness, core height, grid spacing, rib width and material properties on structural stiffness were investigated for the design of sandwich structures with hybrid core. The parameter studies demonstrated that core height had the most significant influence on the specific bending stiffness, while grid spacing was most important for specific in-plane stiffness of sandwich panels with carbon-fiber grid. Moreover, using carbon-fiber grid, although increases manufacturing cost, could further enhance the specific stiffness.


2008 ◽  
Vol 33-37 ◽  
pp. 1233-1240
Author(s):  
Hua Rui Liu ◽  
Q.H. Xu ◽  
J.L. Yang

This paper is disserted to the vibrations of the sandwich panels with pyramidal truss cores. Firstly, based on the Hamilton principle the governing equations of a sandwich panel with pyramidal truss cores are obtained and the eigenfrequencies of the sandwich panel is studied. Then the dynamic response of the sandwich subjected to uniformly distributed sinusoidal loading is studied. The influences of the sizes of the panel on the eigenfrequencies of the panel are discussed. The maximum deflections of the panels of equal mass subjected to the same loading are compared.


2016 ◽  
Vol 148 ◽  
pp. 85-96 ◽  
Author(s):  
Jin-Shui Yang ◽  
Li Ma ◽  
Rüdiger Schmidt ◽  
Ge Qi ◽  
Kai-Uwe Schröder ◽  
...  

2018 ◽  
Vol 200 ◽  
pp. 886-909 ◽  
Author(s):  
H. Yazdani Sarvestani ◽  
A.H. Akbarzadeh ◽  
H. Niknam ◽  
K. Hermenean

2017 ◽  
Vol 172 ◽  
pp. 628-633 ◽  
Author(s):  
Labans Edgars ◽  
Zudrags Kaspars ◽  
Kalnins Kaspars

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