| Article ID | Journal | Published Year | Pages | File Type |
|---|---|---|---|---|
| 10644565 | Computational Materials Science | 2005 | 8 Pages |
Abstract
The present study investigates the method of structural analysis and failure prediction of tape-wrapped structures that have been used in the conventional nozzle structures of rockets. Four-point bending test and its finite element analysis were performed to study how to model tape-wrapped structures and to investigate the failure characteristics of tape-wrapped structures. For dynamic characteristics, the natural frequencies of an inclined stacked plate and a tape-wrapped cylinder were measured and compared with the analytical characteristics.
Related Topics
Physical Sciences and Engineering
Engineering
Computational Mechanics
Authors
Nam Seo Goo, Kwang J. Yoon, Seok Heo,