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Buckling behavior of composite cylinders subjected to compressive loading
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Carri, R. L. |
| Copyright Year | 1973 |
| Description | Room temperature compressive buckling strengths of eight cylinders, four boron-epoxy and four boron-epoxy reinforced-titanium, with diameter to thickness ratios ranging between 40 and 67 are determined experimentally and compared with analytical predictions. Numerical buckling strengths are presented for Donnell's, Flugge's and Sanders' shell theories for anisotropic and orthotropic material cases. Comparison of analytical predictions with experimental results indicates good agreement and the recommended correlation factor suggested in the literature is applicable for design. For the cylinders tested, the correlation between experiment and theory ranged from 0.73 to 0.97. |
| File Size | 1920130 |
| Page Count | 48 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19730021213 |
| Archival Resource Key | ark:/13960/t7kq2s32t |
| Language | English |
| Publisher Date | 1973-06-01 |
| Access Restriction | Open |
| Subject Keyword | Structural Mechanics Correlation Composite Materials Titanium Borides Orthotropic Cylinders Compression Loads Compressive Strength Boron Compounds Buckling 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 |
