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Structural design criteria for filament-wound composite shells
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Claus, S. J. Hipp, P. A. Pai, S. P. Jensen, D. W. Hahn, H. T. |
| Copyright Year | 1994 |
| Description | Advanced composite cylinders, manufactured by filament winding, provide a cost effective solution to many present structural applications; however, the compressive performance of filament-wound cylinders is lower than comparable shells fabricated from unidirectional tape. The objective of this study was to determine the cause of this reduction in thin filament-wound cylinders by relating the manufacturing procedures to the quality of the cylinder and to its compressive performance. The experiments on cylinder buckling were complemented by eigenvalue buckling analysis using a detailed geometric model in a finite element analysis. The applicability of classical buckling analyses was also investigated as a design tool. |
| File Size | 11563523 |
| Page Count | 182 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19940019929 |
| Archival Resource Key | ark:/13960/t90916787 |
| Language | English |
| Publisher Date | 1994-01-01 |
| Access Restriction | Open |
| Subject Keyword | Composite Materials Compression Tests Compression Loads Fiber Composites Filament Winding Defects Finite Element Method Cylindrical Shells Eigenvalues Structural Design Criteria Manufacturing Composite Structures Microstructure Buckling Structural Analysis 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 |
