Axial Compression of Empty and Foam Filled Composite Conical Shells

1999 ◽  
Vol 33 (6) ◽  
pp. 567-591 ◽  
Author(s):  
N. K. Gupta ◽  
R. Velmurugan
Keyword(s):  
Axial Compression ◽  
Conical Shells ◽  
Foam Filled ◽  
Filled Composite

scholarly journals On the Crush Behavior of an Ultra Light Multi-Cell Foam-Filled Composite Structure under Axial Compression

2008 ◽  
Vol 29 (3) ◽  
pp. 391-408 ◽  
Author(s):  
Siavash T. Taher ◽  
Azim A. Oshkour ◽  
Rizal Zahari ◽  
Faizal Mustapha ◽  
Shahnor Basri
Keyword(s):  
Axial Compression ◽  
Composite Structure ◽  
Foam Filled ◽  
Filled Composite ◽  
Cell Foam

scholarly journals A double-cell foam-filled composite block for efficient energy absorption under axial compression

2009 ◽  
Vol 89 (3) ◽  
pp. 399-407 ◽  
Author(s):  
Siavash T. Taher ◽  
Rizal Zahari ◽  
Simin Ataollahi ◽  
Faizal Mustapha ◽  
ShahNor Basri
Keyword(s):  
Energy Absorption ◽  
Axial Compression ◽  
Efficient Energy ◽  
Foam Filled ◽  
Filled Composite ◽  
Cell Foam

Low Buckling Loads of Axially Compressed Conical Shells

1970 ◽  
Vol 37 (2) ◽  
pp. 384-392 ◽  
Author(s):  
M. Baruch ◽  
O. Harari ◽  
J. Singer
Keyword(s):  
Boundary Conditions ◽  
Axial Compression ◽  
Plane Boundary ◽  
Essential Difference ◽  
Physical Reason ◽  
Buckling Loads ◽  
Conical Shells ◽  
Simple Supports ◽  
Interaction Curves ◽  
The Stability

The stability of simply supported conical shells under axial compression is investigated for 4 different sets of in-plane boundary conditions with a linear Donnell-type theory. The first two stability equations are solved by the assumed displacement, while the third is solved by a Galerkin procedure. The boundary conditions are satisfied with 4 unknown coefficients in the expression for u and v. Both circumferential and axial restraints are found to be of primary importance. Buckling loads about half the “classical” ones are obtained for all but the stiffest simple supports SS4 (v = u = 0). Except for short shells, the effects do not depend on the length of the shell. The physical reason for the low buckling loads in the SS3 case is explained and the essential difference between cylinder and cone in this case is discussed. Buckling under combined axial compression and external or internal pressure is studied and interaction curves have been calculated for the 4 sets of in-plane boundary conditions.

Free vibration and buckling of foam-filled composite corrugated sandwich plates under thermal loading

2017 ◽  
Vol 172 ◽  
pp. 173-189 ◽  
Author(s):  
Bin Han ◽  
Ke-Ke Qin ◽  
Qian-Cheng Zhang ◽  
Qi Zhang ◽  
Tian Jian Lu ◽  
...  
Keyword(s):  
Free Vibration ◽  
Thermal Loading ◽  
Sandwich Plates ◽  
Foam Filled ◽  
Filled Composite

Dynamic failure of ceramic particle reinforced foam-filled composite lattice core

2020 ◽  
Vol 193 ◽  
pp. 108143 ◽  
Author(s):  
Wei Huang ◽  
Hongjian Xu ◽  
Zihao Fan ◽  
Weimin Jiang ◽  
Jiayi Liu
Keyword(s):  
Ceramic Particle ◽  
Dynamic Failure ◽  
Foam Filled ◽  
Composite Lattice ◽  
Lattice Core ◽  
Filled Composite

Prediction of the mean folding force during the axial compression in foam-filled grooved tubes by theoretical analysis

2012 ◽  
Vol 37 ◽  
pp. 144-151 ◽  
Author(s):  
Abbas Niknejad ◽  
Mohammad Mahdi Abedi ◽  
Gholam Hossein Liaghat ◽  
Mohammad Zamani Nejad
Keyword(s):  
Theoretical Analysis ◽  
Axial Compression ◽  
Foam Filled ◽  
The Mean
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