NASA NTRS ยท 19760024210
Multi-Fiber Composites
Abstract
Resin matrix composites having improved resistance to foreign object damage in gas turbine engine fan blade applications were developed. Materials evaluated include epoxy matrix graphite/glass and boron/glass hybrids, thermoplastic matrix boron/glass hybrids, and superhybrids consisting of graphite/epoxy, boron/aluminum, and titanium alloy sheets. Static, pendulum impact, and ballistic impact test results are reported for all materials. Superhybrid blade like specimens are shown to be capable of withstanding relatively severe ballistic impacts from gelatin spheres without fracture. The effects of ply configuration and projectile angle of incidence on impact behavior are described. Predictions of surface strains during ballistic impact are presented and shown to be in reasonable agreement with experimental measurements.
Keep this discovery
Explore connections, maps & timelines
Novak, R. C.. 1976-04-01. Multi-Fiber Composites. https://ntrs.nasa.gov/citations/19760024210
Cite the original work for its findings. Save a collection to share your selection of sources.