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.
Optimum Design of Swept-Forward High-Aspect-Ration Graphite-Epoxy Wings
1989
17 pages
Report
No indication
English
Aeroelastic properties of straight and forward swept graphite/epoxy wings
Tema Archive | 1983
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