NASA NTRS · 19910004133
Composite fuselage technology
Abstract
The overall objective is to identify and understand, via directed experimentation and analysis, the mechanisms which control the structural behavior of fuselages in their response to damage (resistance, tolerance, and arrest). A further objective is to develop straightforward design methodologies which can be employed by structural designers in preliminary design stages to make intelligent choices concerning the material, layup, and structural configuration so that a more efficient structure with structural integrity can be designed and built.
Keep this discovery
Explore connections, maps & timelines
Graves, Michael J., Lagace, Paul A.. 1990-10-01. Composite fuselage technology. https://ntrs.nasa.gov/citations/19910004133
Cite the original work for its findings. Save a collection to share your selection of sources.