| contributor author | J. Katz | |
| contributor author | R. Largman | |
| date accessioned | 2017-05-08T23:30:22Z | |
| date available | 2017-05-08T23:30:22Z | |
| date copyright | March, 1989 | |
| date issued | 1989 | |
| identifier issn | 0098-2202 | |
| identifier other | JFEGA4-27040#93_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/105606 | |
| description abstract | The aerodynamic performance of a two-element airfoil with a 90 deg. trailing edge flap was experimentally investigated. The 5 percent-chord long flap, significantly increased the lift of the baseline airfoil, throughout a wide range of angles of attack. The maximum lift coefficient of the flapped wing increased too, whereas the lift/drag ratio decreased. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Effect of 90 Degree Flap on the Aerodynamics of a Two-Element Airfoil | |
| type | Journal Paper | |
| journal volume | 111 | |
| journal issue | 1 | |
| journal title | Journal of Fluids Engineering | |
| identifier doi | 10.1115/1.3243605 | |
| journal fristpage | 93 | |
| journal lastpage | 94 | |
| identifier eissn | 1528-901X | |
| keywords | Aerodynamics | |
| keywords | Airfoils | |
| keywords | Drag (Fluid dynamics) | |
| keywords | Chords (Trusses) AND Wings | |
| tree | Journal of Fluids Engineering:;1989:;volume( 111 ):;issue: 001 | |
| contenttype | Fulltext | |
