Boundary Layer Calculation for Analysis and DesignSource: Journal of Fluids Engineering:;1978:;volume( 100 ):;issue: 002::page 232Author:H. E. Weber
DOI: 10.1115/1.3448637Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: A simple, semiempirical method for calculating the laminar, transition, and turbulent boundary layer with arbitrary free stream pressure gradient is developed. Good correlation is obtained with data on general two dimensional turbulent flows, diffuser flows, and the cylinder in cross-flow. However only for the diffuser has the boundary layer flow been coupled with the potential core so that only the inlet conditions and geometry are required. In other cases the free stream velocity distribution must be known or calculable. Skin friction coefficient, momentum thickness Reynolds number, and free stream pressure gradient parameter correlation employs a simple lag theory. With the integral momentum equation the complete boundary layer parameters are obtained as functions of the distance along a surface.
keyword(s): Boundary layers , Design , Momentum , Flow (Dynamics) , Pressure gradient , Diffusers , Thickness , Cross-flow , Turbulence , Reynolds number , Skin friction (Fluid dynamics) , Boundary layer turbulence , Cylinders , Equations , Functions AND Geometry ,
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| contributor author | H. E. Weber | |
| date accessioned | 2017-05-08T23:05:06Z | |
| date available | 2017-05-08T23:05:06Z | |
| date copyright | June, 1978 | |
| date issued | 1978 | |
| identifier issn | 0098-2202 | |
| identifier other | JFEGA4-26933#232_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/91197 | |
| description abstract | A simple, semiempirical method for calculating the laminar, transition, and turbulent boundary layer with arbitrary free stream pressure gradient is developed. Good correlation is obtained with data on general two dimensional turbulent flows, diffuser flows, and the cylinder in cross-flow. However only for the diffuser has the boundary layer flow been coupled with the potential core so that only the inlet conditions and geometry are required. In other cases the free stream velocity distribution must be known or calculable. Skin friction coefficient, momentum thickness Reynolds number, and free stream pressure gradient parameter correlation employs a simple lag theory. With the integral momentum equation the complete boundary layer parameters are obtained as functions of the distance along a surface. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Boundary Layer Calculation for Analysis and Design | |
| type | Journal Paper | |
| journal volume | 100 | |
| journal issue | 2 | |
| journal title | Journal of Fluids Engineering | |
| identifier doi | 10.1115/1.3448637 | |
| journal fristpage | 232 | |
| journal lastpage | 236 | |
| identifier eissn | 1528-901X | |
| keywords | Boundary layers | |
| keywords | Design | |
| keywords | Momentum | |
| keywords | Flow (Dynamics) | |
| keywords | Pressure gradient | |
| keywords | Diffusers | |
| keywords | Thickness | |
| keywords | Cross-flow | |
| keywords | Turbulence | |
| keywords | Reynolds number | |
| keywords | Skin friction (Fluid dynamics) | |
| keywords | Boundary layer turbulence | |
| keywords | Cylinders | |
| keywords | Equations | |
| keywords | Functions AND Geometry | |
| tree | Journal of Fluids Engineering:;1978:;volume( 100 ):;issue: 002 | |
| contenttype | Fulltext |