NASA NTRS · 19760014203
Filament-wound spar shell graphite/epoxy fan blades
Abstract
The methodology for fabrication of wet filament wound spar shell fan blades is presented. All principal structural elements were filament wound, assembled, formed, bonded and co-cured in a female mold. A pair of blades were fabricated as one integral unit and parted into two after curing.
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Yao, S.. 1976-02-01. Filament-wound spar shell graphite/epoxy fan blades. https://ntrs.nasa.gov/citations/19760014203
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