| contributor author | D. M. Tang | |
| contributor author | M. Q. Wang | |
| date accessioned | 2017-05-08T23:19:09Z | |
| date available | 2017-05-08T23:19:09Z | |
| date copyright | April, 1984 | |
| date issued | 1984 | |
| identifier issn | 1048-9002 | |
| identifier other | JVACEK-28961#235_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/99204 | |
| description abstract | In this paper is introduced a method of dynamic analysis of the helicopter rotor coupled with fuselage in the rotating plane. The method has been used to determine the inplane rotor-fuselage dynamic properties of a light helicopter with fiberglass-reinforced plastics rotor blades. This paper makes particular reference to the effect of anisotropic dynamic stiffness of the rotor shaft end of fuselage on the natural dynamic characteristics. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Coupling Technique of Rotor-Fuselage Dynamic Analysis | |
| type | Journal Paper | |
| journal volume | 106 | |
| journal issue | 2 | |
| journal title | Journal of Vibration and Acoustics | |
| identifier doi | 10.1115/1.3269174 | |
| journal fristpage | 235 | |
| journal lastpage | 238 | |
| identifier eissn | 1528-8927 | |
| keywords | Dynamic analysis | |
| keywords | Rotors | |
| keywords | Blades | |
| keywords | Stiffness | |
| keywords | Plastics AND Glass reinforced plastics | |
| tree | Journal of Vibration and Acoustics:;1984:;volume( 106 ):;issue: 002 | |
| contenttype | Fulltext | |
