| contributor author | G. W. Rankin | |
| contributor author | K. Sridhar | |
| date accessioned | 2017-05-08T23:05:08Z | |
| date available | 2017-05-08T23:05:08Z | |
| date copyright | March, 1978 | |
| date issued | 1978 | |
| identifier issn | 0098-2202 | |
| identifier other | JFEGA4-26930#55_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/91218 | |
| description abstract | The integral form of the momentum and energy equations, subject to the boundary layer simplifications, are used to obtain an approximate solution for an axisymmetric laminar jet with a uniform profile at the nozzle exit. The solution is expressed in a closed form. The jet flow field is divided into a developing and developed region. In the developing region a potential core is assumed to exist, bounded by an annular free shear layer, Schlichting’s velocity profile for an axisymmetric laminar jet is assumed in the free shear layer. The present solution is compared with existing experimental and analytical results in the developing region. Also a graphical method for determining the potential core radius and the parameters of the assumed Schlichting profile is given. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Developing Region of Laminar Jets With Uniform Exit Velocity Profiles | |
| type | Journal Paper | |
| journal volume | 100 | |
| journal issue | 1 | |
| journal title | Journal of Fluids Engineering | |
| identifier doi | 10.1115/1.3448615 | |
| journal fristpage | 55 | |
| journal lastpage | 59 | |
| identifier eissn | 1528-901X | |
| keywords | Jets | |
| keywords | Shear (Mechanics) | |
| keywords | Momentum | |
| keywords | Boundary layers | |
| keywords | Nozzles AND Equations | |
| tree | Journal of Fluids Engineering:;1978:;volume( 100 ):;issue: 001 | |
| contenttype | Fulltext | |
