Low-Reynolds-Number Turbulent Boundary LayersSource: Journal of Fluids Engineering:;1981:;volume( 103 ):;issue: 004::page 624Author:B. R. White
DOI: 10.1115/1.3241782Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: This paper presents experimental wind-tunnel data that show the universal logarithmic velocity profile for zero-pressure-gradient turbulent boundary layer flows is valid for values of momentum-deficit Reynolds numbers Rθ as low as 600. However, for values of Rθ between 425 and 600, the von Kármán and additive constants vary and are shown to be functions of Rθ and shape factor H. Furthermore, the viscous sublayer in the range 425<Rθ <600 can no longer maintain its characteristically small size. It is forced to grow, due to viscous effects, into a super sublayer (6-9 percent of the boundary layer height) that greatly exceeds conventional predictions of sublayer heights.
keyword(s): Boundary layer turbulence , Functions , Gradients , Shapes , Wind tunnels , Pressure , Momentum , Flow (Dynamics) , Reynolds number AND Boundary layers ,
|
Collections
Show full item record
| contributor author | B. R. White | |
| date accessioned | 2017-05-08T23:11:19Z | |
| date available | 2017-05-08T23:11:19Z | |
| date copyright | December, 1981 | |
| date issued | 1981 | |
| identifier issn | 0098-2202 | |
| identifier other | JFEGA4-26977#624_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/94677 | |
| description abstract | This paper presents experimental wind-tunnel data that show the universal logarithmic velocity profile for zero-pressure-gradient turbulent boundary layer flows is valid for values of momentum-deficit Reynolds numbers Rθ as low as 600. However, for values of Rθ between 425 and 600, the von Kármán and additive constants vary and are shown to be functions of Rθ and shape factor H. Furthermore, the viscous sublayer in the range 425<Rθ <600 can no longer maintain its characteristically small size. It is forced to grow, due to viscous effects, into a super sublayer (6-9 percent of the boundary layer height) that greatly exceeds conventional predictions of sublayer heights. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Low-Reynolds-Number Turbulent Boundary Layers | |
| type | Journal Paper | |
| journal volume | 103 | |
| journal issue | 4 | |
| journal title | Journal of Fluids Engineering | |
| identifier doi | 10.1115/1.3241782 | |
| journal fristpage | 624 | |
| journal lastpage | 630 | |
| identifier eissn | 1528-901X | |
| keywords | Boundary layer turbulence | |
| keywords | Functions | |
| keywords | Gradients | |
| keywords | Shapes | |
| keywords | Wind tunnels | |
| keywords | Pressure | |
| keywords | Momentum | |
| keywords | Flow (Dynamics) | |
| keywords | Reynolds number AND Boundary layers | |
| tree | Journal of Fluids Engineering:;1981:;volume( 103 ):;issue: 004 | |
| contenttype | Fulltext |