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Hole interaction and load introduction effects for compression-loaded laminates with holes
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Shuart, M. J. |
| Copyright Year | 1984 |
| Description | The effects of hole interaction and load introduction for (+ or - 30/90) sub 8 (s) and (+ or - 45) sub 12 (s) laminates with holes was conducted. A hole interaction region was identified in some specimens, and this region was ineffective for carrying load. The membrane stiffness of a specimen with a hole interaction region is less than the membrane stiffness of a similar specimen without a hole interaction region. A load introduction effect that occurs on the sublaminate level was also observed. This effect can cause a nonuniform load diffusion into the interior of the specimen. |
| File Size | 8068183 |
| Page Count | 27 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19840024365 |
| Archival Resource Key | ark:/13960/t8dg1km3g |
| Language | English |
| Publisher Date | 1984-08-01 |
| Access Restriction | Open |
| Subject Keyword | Composite Materials Specimen Geometry Hole Distribution Mechanics Hole Geometry Mechanics Stress Distribution Compression Loads Failure Modes Strain Gages Graphite-epoxy Composites Stiffness Holes Mechanics Stress-strain Diagrams Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
