Loading...
Please wait, while we are loading the content...
Similar Documents
Effect of fiber-matrix debonding on notched strength of titanium metal matrix composites
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Bigelow, C. A. Johnson, W. S. |
| Copyright Year | 1991 |
| Description | Two specimen configuration of a (0/90)2s SCS-6/Ti-15-3 laminate were tested and analyzed: a center hole (CH) specimen and a double edge notch (DEN) specimen. The two specimen configurations failed at similar stress levels. Two analytical techniques, a 3-D finite-element analysis and a macro-micromechanical analysis were used to predict the overall stress-deformation behavior and the notch-tip fiber-matrix interface stresses in both configurations. |
| File Size | 1329214 |
| Page Count | 34 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19910019925 |
| Archival Resource Key | ark:/13960/t6q00402k |
| Language | English |
| Publisher Date | 1991-08-01 |
| Access Restriction | Open |
| Subject Keyword | Composite Materials Stress Analysis Failure Modes Notches Fiber Composites Notch Tests Solid-solid Interfaces Laminates Finite Element Method Micromechanics Fiber Strength Stress Distribution Failure Analysis Reinforcing Fibers Delaminating Fiber-matrix Interfaces Titanium Metal Matrix Composites Fiber Orientation Matrix Materials Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
