Design considerations for composite fuselage structure of commercial transport aircraft
- Author
- Sakata, I. F.
- Published
- Mar 1, 1981.
- Physical Description
- 1 electronic document
- Additional Creators
- Davis, G. W.
Online Version
- hdl.handle.net , Connect to this object online.
- Restrictions on Access
- Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access - Summary
- The structural, manufacturing, and service and environmental considerations that could impact the design of composite fuselage structure for commercial transport aircraft application were explored. The severity of these considerations was assessed and the principal design drivers delineated. Technical issues and potential problem areas which must be resolved before sufficient confidence is established to commit to composite materials were defined. The key issues considered are: definition of composite fuselage design specifications, damage tolerance, and crashworthiness.
- Other Subject(s)
- Collection
- NASA Technical Reports Server (NTRS) Collection.
- Note
- Document ID: 19810013888.
Accession ID: 81N22419.
NASA-CR-159296.
LR-29540. - Terms of Use and Reproduction
- No Copyright.
View MARC record | catkey: 15719365