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Buckling behavior of long anisotropic plates subjected to fully restrained thermal expansion (Document No: 20030020669)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Nemeth, Michael P. |
| Copyright Year | 2003 |
| Description | An approach for synthesizing buckling results and behavior for thin, balanced and unbalanced symmetric laminates that are subjected to uniform heating or cooling and which are fully-restrained against thermal expansion or contraction is presented. This approach uses a nondimensional analysis for infinitely long, flexurally anisotropic plates that are subjected to combined mechanical loads and is based on useful nondimensional parameters. In addition, stiffness-weighted laminate thermal-expansion parameters are derived and used to determine critical temperature changes in terms of physically intuitive mechanical buckling coefficients. The effects of membrane orthotropy and anisotropy are included. Many results are presented for some common laminates that are intended to facilitate a structural designer's transition to the use of the generic buckling design curves that are presented in the paper. Several generic buckling design curves are presented that provide physical insight into buckling response and provide useful design data. Examples are presented that demonstrate the use of generic design curves. The analysis approach and generic results indicate the effects and characteristics of laminate thermal expansion, membrane orthotropy and anisotropy, and flexural orthotropy and anisotropy in a very general, unifying manner. |
| File Size | 4871206 |
| Page Count | 92 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20030020669 |
| Archival Resource Key | ark:/13960/t9t19zk72 |
| Language | English |
| Publisher Date | 2003-02-01 |
| Access Restriction | Open |
| Subject Keyword | Metals And Metallic Materials Structural Design Stress Analysis Cooling Anisotropic Plates Mechanical Properties Dimensionless Numbers Laminates Parameter Identification Thermal Expansion Anisotropy Dimensional Analysis Thermal Buckling Critical Temperature Spacecraft Design Loads Forces Structural Analysis Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |