Experimental verification of a progressive damage model for IM7/5260 laminates subjected to tension-tension fatigue

• 161 Want to read
• 27 Currently reading

Published 1995 by National Aeronautics and Space Administration, National Technical Information Service, distributor in [Washington, D.C, Springfield, Va .
Written in English

Subjects:

• Aircraft structures.,
• Finite element method.,
• Resin matrix composites.,
• Crack propagation.,
• Stiffness.,
• Delaminating.,
• Fiber composites.

---

Edition Notes

Statement	Timothy W. Coats, Charles E. Harris.
Series	NASA-TM -- 111921., NASA technical memorandum -- 111921.
Contributions	Harris, Charles E., United States. National Aeronautics and Space Administration.
The Physical Object
Format	Microform
Pagination	1 v.
ID Numbers
Open Library	OL18121115M

---