| contributor author | Hani B. Ludin | |
| contributor author | Ashraf A. Omar | |
| contributor author | Waqar Asrar | |
| date accessioned | 2017-05-08T21:34:41Z | |
| date available | 2017-05-08T21:34:41Z | |
| date copyright | May 2015 | |
| date issued | 2015 | |
| identifier other | %28asce%29be%2E1943-5592%2E0000002.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/56546 | |
| description abstract | A numerical investigation was undertaken to evaluate the capabilities of a differential spoiler setting (DSS) in modifying the spanwise wing load and reducing the hazard of wake vortices imposed on a following aircraft. Numerical simulations were carried out on a scaled, half-model aircraft under a high lift configuration (HLC) condition for two outboard loading cases and two inboard loading cases in addition to the baseline configuration case. The study has covered the near-wake field and the extended near-wake field regions. The results are presented in terms of velocity contours, vorticity contours, tangential velocity, circulation, and streamlines at several measurement sections downstream, namely, at | |
| publisher | American Society of Civil Engineers | |
| title | Numerical Study of the Effect of Spoiler Configuration on Wake Vortex Alleviation | |
| type | Journal Paper | |
| journal volume | 28 | |
| journal issue | 3 | |
| journal title | Journal of Aerospace Engineering | |
| identifier doi | 10.1061/(ASCE)AS.1943-5525.0000406 | |
| tree | Journal of Aerospace Engineering:;2015:;Volume ( 028 ):;issue: 003 | |
| contenttype | Fulltext | |