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Composite fuselage technology
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Lagace, Paul A. Graves, Michael J. |
| Copyright Year | 1990 |
| Description | The overall objective is to identify and understand, via directed experimentation and analysis, the mechanisms which control the structural behavior of fuselages in their response to damage (resistance, tolerance, and arrest). A further objective is to develop straightforward design methodologies which can be employed by structural designers in preliminary design stages to make intelligent choices concerning the material, layup, and structural configuration so that a more efficient structure with structural integrity can be designed and built. |
| File Size | 1081168 |
| Page Count | 25 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19910004133 |
| Archival Resource Key | ark:/13960/t3130sd8q |
| Language | English |
| Publisher Date | 1990-10-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Finite Element Method Plates Structural Members Tolerances Mechanics Aircraft Construction Materials Graphite-epoxy Composites Project Planning Fuselages Crack Arrest Cylinders Crack Propagation 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 |