| contributor author | Y. K. Lin | |
| date accessioned | 2017-05-08T23:30:45Z | |
| date available | 2017-05-08T23:30:45Z | |
| date copyright | December, 1960 | |
| date issued | 1960 | |
| identifier issn | 0021-8936 | |
| identifier other | JAMCAV-25565#669_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/105833 | |
| description abstract | The determination of the natural frequencies and normal modes of vibration for continuous panels, representing more or less typical fuselage skin-panel construction for modern airplanes, is discussed in this paper. The time-dependent boundary conditions at the supporting stringers are considered. A numerical example is presented, and analytical results for a particular structural configuration agree favorably with available experimental measurements. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Free Vibration of Continuous Skin-Stringer Panels | |
| type | Journal Paper | |
| journal volume | 27 | |
| journal issue | 4 | |
| journal title | Journal of Applied Mechanics | |
| identifier doi | 10.1115/1.3644080 | |
| journal fristpage | 669 | |
| journal lastpage | 676 | |
| identifier eissn | 1528-9036 | |
| keywords | Free vibrations | |
| keywords | Skin | |
| keywords | Frequency | |
| keywords | Measurement | |
| keywords | Construction | |
| keywords | Vibration | |
| keywords | Aircraft AND Boundary-value problems | |
| tree | Journal of Applied Mechanics:;1960:;volume( 027 ):;issue: 004 | |
| contenttype | Fulltext | |
