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Comparison of toughened composite laminates using nasa standard damage tolerance tests
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Chapman II, A. J. Obrien, T. K. Williams, J. G. |
| Copyright Year | 1984 |
| Description | The proposed application of composite materials to transport wing and fuselage structures prompted the search for tougher materials having improved resistance to impact damage and delamination. Several resin/graphite fiber composite materials were subjected to standard damage tolerance tests and the results were compared to ascertain which materials have superior toughness. In addition, test results from various company and NASA laboratories were compared for repeatability. |
| File Size | 2510185 |
| Page Count | 23 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19840021903 |
| Archival Resource Key | ark:/13960/t52g2k23r |
| Language | English |
| Publisher Date | 1984-08-01 |
| Access Restriction | Open |
| Subject Keyword | Composite Materials Structural Design Deformation Compression Tests Aircraft Construction Materials Fiber Composites Aircraft Design Compressive Strength Impact Tests Laminates Impact Loads Tensile Strength Notch Sensitivity Toughness Wings Fuselages Fracture Strength Acee Program Impact Damage Resin Matrix Composites Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
