| contributor author | Wenqing Yang | |
| contributor author | Bifeng Song | |
| contributor author | Liguang Wang | |
| contributor author | Lili Chen | |
| date accessioned | 2017-05-08T22:16:58Z | |
| date available | 2017-05-08T22:16:58Z | |
| date copyright | November 2015 | |
| date issued | 2015 | |
| identifier other | 40078925.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/76118 | |
| description abstract | This paper presents a numerical method to simulate the dynamic interaction between the structural deformation and the aerodynamic characteristics of flexible flapping wing for micro air vehicle (MAV). A fluid-structure coupling solver is developed based on the Navier-Stokes equations and the structural dynamic equations. In addition, the interface data exchange method based on the radial basis function and the moving mesh generation method based on the infinite interpolation are applied, which play an important role in the coupling research. The preceding method is validated by comparison with the wind tunnel experimental results. For the research scope of this article ( | |
| publisher | American Society of Civil Engineers | |
| title | Dynamic Fluid-Structure Coupling Method of Flexible Flapping Wing for MAV | |
| type | Journal Paper | |
| journal volume | 28 | |
| journal issue | 6 | |
| journal title | Journal of Aerospace Engineering | |
| identifier doi | 10.1061/(ASCE)AS.1943-5525.0000490 | |
| tree | Journal of Aerospace Engineering:;2015:;Volume ( 028 ):;issue: 006 | |
| contenttype | Fulltext | |