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Design considerations for composite fuselage structure of commercial transport aircraft
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Davis, G. W. Sakata, I. F. |
| Copyright Year | 1981 |
| Description | The structural, manufacturing, and service and environmental considerations that could impact the design of composite fuselage structure for commercial transport aircraft application were explored. The severity of these considerations was assessed and the principal design drivers delineated. Technical issues and potential problem areas which must be resolved before sufficient confidence is established to commit to composite materials were defined. The key issues considered are: definition of composite fuselage design specifications, damage tolerance, and crashworthiness. |
| File Size | 2059418 |
| Page Count | 51 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19810013888 |
| Archival Resource Key | ark:/13960/t0fv3cz0p |
| Language | English |
| Publisher Date | 1981-03-01 |
| Access Restriction | Open |
| Subject Keyword | Structural Mechanics Structural Design Aircraft Safety Composite Materials Transport Aircraft Aircraft Construction Materials Fuselages Aircraft Design Aeronautical Engineering Aircraft Parts Composite Structures 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 |