| contributor author | Y. K. Lin | |
| contributor author | T. J. McDaniel | |
| date accessioned | 2017-05-09T00:23:40Z | |
| date available | 2017-05-09T00:23:40Z | |
| date copyright | November, 1969 | |
| date issued | 1969 | |
| identifier issn | 1087-1357 | |
| identifier other | JMSEFK-27546#1133_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/135711 | |
| description abstract | An analytical technique is developed for the determination of the frequency response matrix of a one-dimensional periodic structure. The detailed analysis is carried out for a periodic Bernoulli-Euler beam on many elastic supports, a simplified version for a skin-stringer panel system commonly used in flight vehicle designs. It is shown that considerable simplification can be achieved by introducing one of several possible interior singular conditions. Finally, numerical examples are given for an undamped system and for the same system with damper units attached at periodic locations. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Dynamics of Beam-Type Periodic Structures | |
| type | Journal Paper | |
| journal volume | 91 | |
| journal issue | 4 | |
| journal title | Journal of Manufacturing Science and Engineering | |
| identifier doi | 10.1115/1.3591761 | |
| journal fristpage | 1133 | |
| journal lastpage | 1141 | |
| identifier eissn | 1528-8935 | |
| keywords | Periodic structures | |
| keywords | Dynamics (Mechanics) | |
| keywords | Dampers | |
| keywords | Frequency response | |
| keywords | Skin | |
| keywords | Flight AND Automotive design | |
| tree | Journal of Manufacturing Science and Engineering:;1969:;volume( 091 ):;issue: 004 | |
| contenttype | Fulltext | |