Influence of Free-Stream Turbulence on Boundary Layer Transition in Favorable Pressure GradientsSource: Journal of Engineering for Gas Turbines and Power:;1982:;volume( 104 ):;issue: 004::page 743Author:M. F. Blair
DOI: 10.1115/1.3227340Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Results from an experimental study of large-scale, two-dimensional incompressible transitional boundary layer flows are presented. Tests were conducted on a heated flat wall with a zero pressure gradient and for two levels of “sink” streamwise acceleration; k = ν/U2 ∂U/∂x = 0.2 or 0.75 × 10−6 . Free-stream turbulence intensity levels ranged from approximately 0.7 to 5 percent with limited data obtained outside these values. Convective heat-transfer distributions, laminar, transitional, and fully turbulent boundary layer mean velocity and temperature profile data, and free-stream turbulence intensity distributions are presented. Boundary layer integral quantities and shape factors are also given. Transition onset Reynolds number data obtained for this program agreed well with the results of other experimental and theoretical studies for both zero pressure gradient and accelerating flows. Comparisons of the profile data and wall heat-transfer distribution data indicated that fully turbulent mean velocity profiles were achieved upstream of fully turbulent wall heat-transfer rates.
keyword(s): Turbulence , Boundary layers , Pressure gradient , Heat transfer , Flow (Dynamics) , Reynolds number , Shapes , Temperature profiles AND Boundary layer turbulence ,
|
Show full item record
| contributor author | M. F. Blair | |
| date accessioned | 2017-05-08T23:13:08Z | |
| date available | 2017-05-08T23:13:08Z | |
| date copyright | October, 1982 | |
| date issued | 1982 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26777#743_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/95725 | |
| description abstract | Results from an experimental study of large-scale, two-dimensional incompressible transitional boundary layer flows are presented. Tests were conducted on a heated flat wall with a zero pressure gradient and for two levels of “sink” streamwise acceleration; k = ν/U2 ∂U/∂x = 0.2 or 0.75 × 10−6 . Free-stream turbulence intensity levels ranged from approximately 0.7 to 5 percent with limited data obtained outside these values. Convective heat-transfer distributions, laminar, transitional, and fully turbulent boundary layer mean velocity and temperature profile data, and free-stream turbulence intensity distributions are presented. Boundary layer integral quantities and shape factors are also given. Transition onset Reynolds number data obtained for this program agreed well with the results of other experimental and theoretical studies for both zero pressure gradient and accelerating flows. Comparisons of the profile data and wall heat-transfer distribution data indicated that fully turbulent mean velocity profiles were achieved upstream of fully turbulent wall heat-transfer rates. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Influence of Free-Stream Turbulence on Boundary Layer Transition in Favorable Pressure Gradients | |
| type | Journal Paper | |
| journal volume | 104 | |
| journal issue | 4 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.3227340 | |
| journal fristpage | 743 | |
| journal lastpage | 750 | |
| identifier eissn | 0742-4795 | |
| keywords | Turbulence | |
| keywords | Boundary layers | |
| keywords | Pressure gradient | |
| keywords | Heat transfer | |
| keywords | Flow (Dynamics) | |
| keywords | Reynolds number | |
| keywords | Shapes | |
| keywords | Temperature profiles AND Boundary layer turbulence | |
| tree | Journal of Engineering for Gas Turbines and Power:;1982:;volume( 104 ):;issue: 004 | |
| contenttype | Fulltext |