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Evaluation of bonded boron/epoxy doublers for commercial aircraft aluminum structures
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Belason, Bruce Rutherford, Paul Raj, Shreeram Miller, Matthew |
| Copyright Year | 1994 |
| Description | An 18 month laboratory test and stress analysis program was conducted to evaluate bonded boron/epoxy doublers for repairing cracks on aluminum aircraft structures. The objective was to obtain a core body of substantiating data which will support approval for use on commercial transports of a technology that is being widely used by the military. The data showed that the doublers had excellent performance. |
| File Size | 681779 |
| Page Count | 12 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19950008043 |
| Archival Resource Key | ark:/13960/t5jb13330 |
| Language | English |
| Publisher Date | 1994-09-01 |
| Access Restriction | Open |
| Subject Keyword | Structural Mechanics Fatigue Life Stress-strain Relationships Boron-epoxy Composites Airframes Aluminum Commercial Aircraft Maintainability Aircraft Structures Certification Crack Propagation Structural Analysis Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |