| contributor author | Mario Lee | |
| contributor author | Chih-Ming Ho | |
| date accessioned | 2017-05-08T23:31:34Z | |
| date available | 2017-05-08T23:31:34Z | |
| date copyright | September, 1990 | |
| date issued | 1990 | |
| identifier issn | 0003-6900 | |
| identifier other | AMREAD-25592#209_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/106310 | |
| description abstract | On a delta wing, the separation vorticies can be stationary due to the balance of the vorticity surface flux and the axial convection along the swept leading edge. These stationary vortices keep the wing from losing lift. A highly swept delta wing reaches the maximum lift at an angle of attack of about 40°, which is more than twice as high as that of a two-dimensional airfoil. In this paper, the experimental results of lift forces for delta wings are reviewed from the perspective of fundamental vorticity balance. The effects of different operational and geometrical parameters on the performance of delta wings are surveyed. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Lift Force of Delta Wings | |
| type | Journal Paper | |
| journal volume | 43 | |
| journal issue | 9 | |
| journal title | Applied Mechanics Reviews | |
| identifier doi | 10.1115/1.3119169 | |
| journal fristpage | 209 | |
| journal lastpage | 221 | |
| identifier eissn | 0003-6900 | |
| keywords | Lift (Fluid dynamics) | |
| keywords | Wings | |
| keywords | Vorticity | |
| keywords | Convection | |
| keywords | Vortices | |
| keywords | Airfoils AND Separation (Technology) | |
| tree | Applied Mechanics Reviews:;1990:;volume( 043 ):;issue: 009 | |
| contenttype | Fulltext | |