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Out of plane gradients in laminated composites
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Herakovich, Carl T. |
| Copyright Year | 1994 |
| Description | The research under this grant focused on three different, but related, research projects. All three projects were concerned with predicting the interlaminar stresses that develop in laminated composites in the presence of free edges. The first project was dedicated to the development of a new semi-analytical approximate solution for predicting interlaminar stresses. The second project was devoted to a study of the influence of boundary conditions, geometric parameters, and material modelling on interlaminar stresses in stiffened composite panels. The third project was dedicated to the development of a new finite element for efficient analysis of interlaminar stresses in curved, stiffened panels. A summary of each of the projects is given. |
| File Size | 160768 |
| Page Count | 4 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19940019093 |
| Archival Resource Key | ark:/13960/t44r2tf07 |
| Language | English |
| Publisher Date | 1994-01-20 |
| Access Restriction | Open |
| Subject Keyword | Composite Materials Panels Stress Analysis Approximation Interlaminar Stress Flat Plates Reinforcement Structures Curved Panels Boundary Conditions Stiffening Laminates Finite Element Method Plane Strain Reinforced Plates Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |