Chandrashekhara, K and Bhimaraddi, A (1983) Comparison of Elasticity, Shell Core, and Sandwich Shell Theories. In: AIAA Journal, 21 (1). pp. 114-119.Full text not available from this repository. (Request a copy)
The problem of an infinite circular sandwich shell subjected to an a\isymmetric radial line load is investigated using three-dimensional elasticity theory, shell core method, and sandwich shell theory due to Fulton and Schmidt. A comparison of the stresses and displacements with an exact elasticity solution is carried out for various shell parameters in order to clearly bring out the limitations of sandwich shell theories of Fulton and Schmidt as well as the shell core solution.
|Item Type:||Journal Article|
|Additional Information:||Copyright of this article belongs to American Institute of Aeronautics and Astronautics.|
|Department/Centre:||Division of Mechanical Sciences > Civil Engineering|
|Date Deposited:||14 Jul 2009 14:04|
|Last Modified:||14 Jul 2009 14:04|
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