| contributor author | Saeed Jamei | |
| contributor author | Adi Maimun | |
| contributor author | Shuhaimi Mansor | |
| contributor author | Nor Azwadi | |
| contributor author | Agoes Priyanto | |
| date accessioned | 2017-05-08T21:34:35Z | |
| date available | 2017-05-08T21:34:35Z | |
| date copyright | January 2016 | |
| date issued | 2016 | |
| identifier other | %28asce%29as%2E1943-5525%2E0000383.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/56525 | |
| description abstract | The configuration and service condition of a wing can influence the performance of wing-in-ground effect (WIG) craft. In this study, the aerodynamic performance of compound wings in ground effect was numerically investigated through a parametric design study. The compound wing is divided into three parts with one rectangular wing in the middle and two reverse taper wings with an anhedral angle at the sides. A NACA6409 airfoil was employed as a section of the wing. The design parameters included the span size, anhedral angle, and taper ratio plus two boundary conditions: ground clearance and Reynolds number. The three-dimensional, Reynolds-averaged Navier-Stokes (RANS) equations were solved numerically. A realizable | |
| publisher | American Society of Civil Engineers | |
| title | Design Parametric Study of a Compound Wing-in-Ground Effect. I: Aerodynamics Performance | |
| type | Journal Paper | |
| journal volume | 29 | |
| journal issue | 1 | |
| journal title | Journal of Aerospace Engineering | |
| identifier doi | 10.1061/(ASCE)AS.1943-5525.0000380 | |
| tree | Journal of Aerospace Engineering:;2016:;Volume ( 029 ):;issue: 001 | |
| contenttype | Fulltext | |
