| contributor author | Konstantin I. Matveev | |
| date accessioned | 2017-05-08T21:33:50Z | |
| date available | 2017-05-08T21:33:50Z | |
| date copyright | April 2012 | |
| date issued | 2012 | |
| identifier other | %28asce%29as%2E1943-5525%2E0000126.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/56270 | |
| description abstract | High-payload platforms flying in extreme-ground-effect represent a promising concept for high-speed amphibious transportation. Their dynamics is governed, to a large extent, by unsteady airflow under the platform. A quasi-one-dimensional model for the underplatform channel-flow is applied to predict heave and pitch motions of a vehicle in the presence of external disturbances, such as nonuniformities on the underlying ground-surface. It is found that a complete nonlinear theory should be used instead of a linear model to accurately predict motions when ground nonuniformities are relatively short. A flat platform with a flap moving in extreme-ground-effect is intrinsically unstable. An aft-wing out of ground-effect can be added to the system to achieve stability. Movable control surfaces, such as a platform flap, can be also modeled by the nonlinear theory. It is demonstrated that an oscillating flap can reduce heave and pitch amplitudes in flight over a wavy ground-surface. | |
| publisher | American Society of Civil Engineers | |
| title | Heave-Pitch Motions of a Platform Flying in Extreme Ground Effect | |
| type | Journal Paper | |
| journal volume | 25 | |
| journal issue | 2 | |
| journal title | Journal of Aerospace Engineering | |
| identifier doi | 10.1061/(ASCE)AS.1943-5525.0000126 | |
| tree | Journal of Aerospace Engineering:;2012:;Volume ( 025 ):;issue: 002 | |
| contenttype | Fulltext | |