Loading...
Please wait, while we are loading the content...
Similar Documents
Buckling of fiber reinforced composite plates with nanofiber reinforced matrices
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Murthy, Pappu L. N. Chamis, Christos C. |
| Copyright Year | 2010 |
| Description | Anisotropic composite plates were evaluated with nanofiber reinforced matrices (NFRM). The nanofiber reinforcement volumes ratio in the matrix was 0.01. The plate dimensions were 20 by 10 by 1.0 in. (508 by 254 by 25.4 mm). Seven different loading condition cases were evaluated: three for uniaxial loading, three for pairs of combined loading, and one with three combined loadings. The anisotropy arose from the unidirectional plates having been at 30 from the structural axis. The anisotropy had a full 6 by 6 rigidities matrix which were satisfied and solved by a Galerkin buckling algorithm. The buckling results showed that the NFRM plates buckled at about twice those with conventional matrix. |
| File Size | 1527100 |
| Page Count | 13 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20120002748 |
| Archival Resource Key | ark:/13960/t4zh1mn1k |
| Language | English |
| Publisher Date | 2010-10-03 |
| Access Restriction | Open |
| Subject Keyword | Composite Materials Anisotropic Plates Plates Structural Members Fiber Composites Reinforced Plates Stiffness Galerkin Method Buckling Convergence Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
