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A finite-difference program for stresses in anisotropic, layered plates in bending
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Salamon, N. J. |
| Copyright Year | 1975 |
| Description | The interlaminar stresses induced in a layered laminate that is bent into a cylindrical surface are studied. The laminate is modeled as a continuum, and the resulting elasticity equations are solved using the finite difference method. The report sets forth the mathematical framework, presents some preliminary results, and provides a listing and explanation of the computer program. Significant among the results are apparent symmetry relationships that will reduce the numerical size of certain problems and an interlaminar stress behavior having a sharp rise at the free edges. |
| File Size | 2524705 |
| Page Count | 87 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19750023454 |
| Archival Resource Key | ark:/13960/t2w42j33z |
| Language | English |
| Publisher Date | 1975-09-01 |
| Access Restriction | Open |
| Subject Keyword | Structural Mechanics Computer Programming Stress Analysis Composite Materials Plates Structural Members Finite Difference Theory Bending Mathematical Models Laminates Elastic Deformation Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
