Combined-load stress-strain relationship for advanced fiber composites
- Author
- Sullivan, T. L.
- Published
- JAN 1, 1975.
- Physical Description
- 1 electronic document
- Additional Creators
- Chamis, C. C.
Online Version
- hdl.handle.net , Connect to this object online.
- Restrictions on Access
- Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access - Summary
- It was demonstrated experimentally that only one test specimen is required to determine the combined-load stress-strain relationships of a given fiber composite system. These relationships were determined using a thin angle-plied laminate tube and subjecting it to a number of combined-loading conditions. The measured data obtained are compared with theoretical predictions. Some important considerations associated with such a test are identified, and the significance of combined-load stress-strain relationships in certain practical designs are discussed.
- Other Subject(s)
- Collection
- NASA Technical Reports Server (NTRS) Collection.
- Note
- Document ID: 19760005054.
Accession ID: 76N12142.
E-8526.
NASA-TM-X-71825.
Ann. Reinforced Plastics Composites Conf.; 3-6 Feb. 1976; Washington, DC; United States. - Terms of Use and Reproduction
- No Copyright.
View MARC record | catkey: 15737952