| contributor author | Amin Boukenkoul, Mohammed | |
| contributor author | Li, Feng-Chen | |
| contributor author | Chen, Wen-Li | |
| contributor author | Zhang, Hong-Na | |
| date accessioned | 2019-02-28T10:59:12Z | |
| date available | 2019-02-28T10:59:12Z | |
| date copyright | 9/20/2017 12:00:00 AM | |
| date issued | 2018 | |
| identifier issn | 0098-2202 | |
| identifier other | fe_140_01_011104.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4251441 | |
| description abstract | Despite the big interest in both, micro-air vehicles (MAV) and flow-control strategies, only few studies have investigated the flow-control possibilities over low aspect ratio (LAR) wings flying at low Reynolds numbers (Re). The present study verified the LAR thick airfoils' conformity with the nonlinear lift approximation equation. Then, a moving-wall flow control method was designed and tested over an LAR thick airfoil (0.57 aspect ration (AR), NACA0015 shaped) performing at a chord-based Re of 4 × 104. The moving belt control postponed the stall onset by 25 deg and produced a 103% gain in lift without any saturation signs at a control speed ratio of Ub/U = 6. Particle image velocimetry (PIV) measurements confirmed the effectiveness of the moving-wall control strategy on the upper surface flow reattachment. Moreover, other quantities such as the, vortices, and the swirling strength are investigated. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Lift-Generation and Moving-Wall Flow Control Over a Low Aspect Ratio Airfoil | |
| type | Journal Paper | |
| journal volume | 140 | |
| journal issue | 1 | |
| journal title | Journal of Fluids Engineering | |
| identifier doi | 10.1115/1.4037681 | |
| journal fristpage | 11104 | |
| journal lastpage | 011104-10 | |
| tree | Journal of Fluids Engineering:;2018:;volume( 140 ):;issue: 001 | |
| contenttype | Fulltext | |
