| contributor author | S. G. Lekoudis | |
| date accessioned | 2017-05-08T23:09:00Z | |
| date available | 2017-05-08T23:09:00Z | |
| date copyright | December, 1980 | |
| date issued | 1980 | |
| identifier issn | 0098-2202 | |
| identifier other | JFEGA4-26964#502_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/93444 | |
| description abstract | The problem of the propagation of three-dimensional laminar instabilities, due to crossflow, in a three-dimensional compressible boundary layer, is examined using linear theory. The theory is applied to the case of a transonic swept wing. It is shown that compressibility has a mild stabilizing effect in the regions where the crossflow is strong. The problem of defining the direction of propagation of the disturbances is discussed. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | The Linear Instability Due to the Compressible Crossflow on a Swept Wing | |
| type | Journal Paper | |
| journal volume | 102 | |
| journal issue | 4 | |
| journal title | Journal of Fluids Engineering | |
| identifier doi | 10.1115/1.3240734 | |
| journal fristpage | 502 | |
| journal lastpage | 509 | |
| identifier eissn | 1528-901X | |
| keywords | Wings | |
| keywords | Compressibility AND Boundary layers | |
| tree | Journal of Fluids Engineering:;1980:;volume( 102 ):;issue: 004 | |
| contenttype | Fulltext | |
