| contributor author | M. J. Werle | |
| contributor author | G. D. Senechal | |
| date accessioned | 2017-05-09T01:35:48Z | |
| date available | 2017-05-09T01:35:48Z | |
| date copyright | September, 1973 | |
| date issued | 1973 | |
| identifier issn | 0021-8936 | |
| identifier other | JAMCAV-25989#679_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/163413 | |
| description abstract | A numerical study has been made of the nature of the solution to the supersonic boundary-layer equations when the flow separates from the surface. To this end, implicit finite-difference solutions to the governing equations were obtained for linearly and quadratically retarded flows over flat plates for a Mach number range of 2–15. Both extremely hot and cold-wall conditions are considered. The resutls of this study give strong evidence that all noninteracting flows are singular at separation. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | A Numerical Study of Separating Supersonic Laminar Boundary Layers | |
| type | Journal Paper | |
| journal volume | 40 | |
| journal issue | 3 | |
| journal title | Journal of Applied Mechanics | |
| identifier doi | 10.1115/1.3423072 | |
| journal fristpage | 679 | |
| journal lastpage | 684 | |
| identifier eissn | 1528-9036 | |
| keywords | Boundary layers | |
| keywords | Flow (Dynamics) | |
| keywords | Equations | |
| keywords | Flat plates | |
| keywords | Mach number AND Separation (Technology) | |
| tree | Journal of Applied Mechanics:;1973:;volume( 040 ):;issue: 003 | |
| contenttype | Fulltext | |
