| contributor author | D. Yadav | |
| contributor author | R. P. Ramamoorthy | |
| date accessioned | 2017-05-08T23:34:58Z | |
| date available | 2017-05-08T23:34:58Z | |
| date copyright | December, 1991 | |
| date issued | 1991 | |
| identifier issn | 0022-0434 | |
| identifier other | JDSMAA-26176#677_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/108230 | |
| description abstract | Landing gear dynamics for an aircraft has been analyzed with a heave-pitch model having telescopic main gear and articulated nose gear using oleopneumatic shock absorber. System equations have been presented incorporating the effects of linkage dynamics, frictional forces, and nonlinearities in the tyre, air spring, and oleo damping forces. Sensitivity of the system response to variations in some shock strut parameters has been investigated for the landing touchdown impact phase to bring about improvement in the performance. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Nonlinear Landing Gear Behavior at Touchdown | |
| type | Journal Paper | |
| journal volume | 113 | |
| journal issue | 4 | |
| journal title | Journal of Dynamic Systems, Measurement, and Control | |
| identifier doi | 10.1115/1.2896474 | |
| journal fristpage | 677 | |
| journal lastpage | 683 | |
| identifier eissn | 1528-9028 | |
| keywords | Gears | |
| keywords | Dynamics (Mechanics) | |
| keywords | Force | |
| keywords | Shock (Mechanics) | |
| keywords | Struts (Engineering) | |
| keywords | Linkages | |
| keywords | Damping | |
| keywords | Aircraft | |
| keywords | Equations | |
| keywords | Shock absorbers | |
| keywords | Springs AND Tires | |
| tree | Journal of Dynamic Systems, Measurement, and Control:;1991:;volume( 113 ):;issue: 004 | |
| contenttype | Fulltext | |
