| contributor author | James A. Miller | |
| date accessioned | 2017-05-09T00:18:44Z | |
| date available | 2017-05-09T00:18:44Z | |
| date copyright | October, 1969 | |
| date issued | 1969 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26681#239_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/133112 | |
| description abstract | Measurements of local heat-transfer coefficients in the fully established oscillating turbulent boundary layer over a flat plate are reported. In the range of frequencies from 0.1 to 200 cps and amplitudes from 8 to 92 percent of the freestream mean velocity, increases in local Nusselt numbers of 3 to 5 percent were found. It is concluded that substantial increases in local coefficients, sometimes reported in oscillating flows of low standing wave ratio, may be traced to reduced transition Reynolds numbers. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Heat Transfer in the Oscillating Turbulent Boundary Layer | |
| type | Journal Paper | |
| journal volume | 91 | |
| journal issue | 4 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.3574744 | |
| journal fristpage | 239 | |
| journal lastpage | 244 | |
| identifier eissn | 0742-4795 | |
| keywords | Heat transfer | |
| keywords | Boundary layer turbulence | |
| keywords | Flat plates | |
| keywords | Frequency | |
| keywords | Flow (Dynamics) | |
| keywords | Measurement | |
| keywords | Reynolds number AND Standing waves | |
| tree | Journal of Engineering for Gas Turbines and Power:;1969:;volume( 091 ):;issue: 004 | |
| contenttype | Fulltext | |