A fuselage structure is described in which the skin is comprised of layers of a matrix fiber reinforced composite, with the stringers reinforced with the same composite material. The high strength to weight ratio of the composite, particularly at elevated temperatures, and its high modulus of elasticity, makes it desirable for use in airplane structures.
Fuselage structure using advanced technology fiber reinforced composites
12.01.1982
Sonstige
Keine Angabe
Englisch
Advanced technology commercial fuselage structure
NTRS | 1991
|Advanced Technology Commercial Fuselage Structure
NTIS | 1991
|Advanced Composite Fuselage Technology
British Library Conference Proceedings | 1992
|Advanced Technology Composite Fuselage: Program Overview
NTRS | 1997
|