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Flight service evaluation of kevlar-49/epoxy composite panels in wide-bodied commercial transport aircraft
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Stone, R. H. |
| Copyright Year | 1977 |
| Description | Kevlar-49 fairing panels, installed as flight service components on three L-1011s, were inspected after three years' service, and found to be performing satisfactorily. There are six Kevlar-49 panels on each aircraft, including sandwich and solid laminate wing-body panels, and 150 C service aft engine fairings. The service history to date indicates that Kevlar-49 epoxy composite materials have satisfactory service characteristics for use in aircraft secondary structure. |
| File Size | 18690575 |
| Page Count | 45 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19770017255 |
| Archival Resource Key | ark:/13960/t4tj39g1g |
| Language | English |
| Publisher Date | 1977-03-01 |
| Access Restriction | Open |
| Subject Keyword | Composite Materials Aircraft Maintenance Transport Aircraft Epoxy Compounds Commercial Aircraft Laminates Composite Structures Sandwich Structures Wing Panels 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 |
