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Fuel containment and damage tolerance for large composite primary aircraft structures. phase 1: testing
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Sandifer, J. P. |
| Copyright Year | 1983 |
| Description | Technical problems associated with fuel containment and damage tolerance of composite material wings for transport aircraft were identified. The major tasks are the following: (1) the preliminary design of damage tolerant wing surface using composite materials; (2) the evaluation of fuel sealing and lightning protection methods for a composite material wing; and (3) an experimental investigation of the damage tolerant characteristics of toughened resin graphite/epoxy materials. The test results, the test techniques, and the test data are presented. |
| File Size | 236138143 |
| Page Count | 522 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19850026928 |
| Archival Resource Key | ark:/13960/t0ms8jv43 |
| Language | English |
| Publisher Date | 1983-03-01 |
| Access Restriction | Open |
| Subject Keyword | Composite Materials Fuel Tanks Wings Yield Point Transport Aircraft Mechanical Properties Graphite-epoxy Composites Damage Resins Aircraft Structures Containment Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
