| contributor author | G. T. Flowers | |
| contributor author | B. H. Tongue | |
| date accessioned | 2017-05-08T23:37:11Z | |
| date available | 2017-05-08T23:37:11Z | |
| date copyright | April, 1991 | |
| date issued | 1991 | |
| identifier issn | 1048-9002 | |
| identifier other | JVACEK-28797#141_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/109506 | |
| description abstract | The term “air resonance” refers to an instability associated with helicopters in hover. It is characterized by a coupling between motions of the fuselage and the blades and is of primary concern for helicopters having soft in-plane rotors. This paper presents a study of the effects of nonlinearities on the dynamical behavior of a simplified air resonance model. In order to provide a direct comparison between the behavior of the linearized system and the nonlinear one, a linear analysis of the air resonance model is first performed. Then, the system is analyzed for the effect of selected nonlinearities on its steady state dynamical responses. Geometric nonlinearities and cubic lag damping are considered in these analyses. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Nonlinear Behavior of a Rotorcraft Model During Air Resonance | |
| type | Journal Paper | |
| journal volume | 113 | |
| journal issue | 2 | |
| journal title | Journal of Vibration and Acoustics | |
| identifier doi | 10.1115/1.2930162 | |
| journal fristpage | 141 | |
| journal lastpage | 151 | |
| identifier eissn | 1528-8927 | |
| keywords | Resonance | |
| keywords | Helicopters | |
| keywords | Steady state | |
| keywords | Motion | |
| keywords | Damping | |
| keywords | Rotors AND Blades | |
| tree | Journal of Vibration and Acoustics:;1991:;volume( 113 ):;issue: 002 | |
| contenttype | Fulltext | |
