Finite Element Formulation Based on the Extended High-Order Sandwich Panel Theory
Author:
Affiliation:
1. Aerospace Engineering, Georgia Institute of Technology, Atlanta, Georgia 30332-0150
2. Structural Engineering, Technion–Israel Institute of Technology, 32000 Haifa, Israel
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J053736
Reference16 articles.
1. Structural and Failure Mechanics of Sandwich Composites
2. The blast resistance of sandwich composites with stepwise graded cores
3. Three-dimensional elasticity solution for sandwich beams/wide plates with orthotropic phases: The negative discriminant case
4. High‐Order Theory for Sandwich‐Beam Behavior with Transversely Flexible Core
5. Analysis of Sandwich Beams With a Compliant Core and With In-Plane Rigidity—Extended High-Order Sandwich Panel Theory Versus Elasticity
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