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Optimum design of swept-forward high-aspect-ration graphite-epoxy wings
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Shuart, Mark J. Haftka, Raphael T. Campbell, R. L. |
| Copyright Year | 1989 |
| Description | An analytical investigation of a swept-forward high-aspect-ratio graphite-epoxy transport wing is described. The objectives of this investigation are to illustrate an effective usage of the unique properties of composite materials by exploiting material tailoring and to demonstrate an integrated multidisciplinary approach for conducting this investigation. |
| File Size | 807003 |
| Page Count | 17 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19890015801 |
| Archival Resource Key | ark:/13960/t0xq1ws0v |
| Language | English |
| Publisher Date | 1989-04-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance High Aspect Ratio X-29 Aircraft Aircraft Construction Materials Aerodynamics Swept Forward Wings Graphite-epoxy Composites Aircraft Design Composite Structures Optimization Structural Analysis Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |