1 |
Han, J. C., 1984, Heat transfer and friction in channels with two opposite rib-roughened walls, ASME J. Heat Transfer, Vol. 106, No. 4, pp. 774-781.
DOI
|
2 |
Han, J. C., Park, J. S., and Lei, C. K., 1985, Heat transfer enhancement in channels with turbulence promotors, ASME J. Engng Gas Turbine Pwr, Vol. 107, No. 3, pp. 629-635.
|
3 |
Han, J. C., 1988, Heat transfer and friction characteristics in rectangular channels with rib turbulators, ASME J. Heat Transfer, Vol. 110, No. 2, pp. 321-328.
DOI
|
4 |
Han, J. C. and Park, J. S., 1988, Developing heat transfer in rectangular channels with rib turbulators, Int. J. Heat Mass Transfer, Vol. 31, No. 1, pp. 183-195.
DOI
|
5 |
Han, J. C. and Zhang, P., 1989, Pressure loww distribution in three-pass rectangular channels with rib turbulators, ASME J. Turbomachinery, Vol. 111, No. 4, pp. 515-521.
DOI
|
6 |
Han, J. C. and Zhang, P., 1991, Effect of rib-angle-orientation on local mass transfer distribution in a three-pass rib-roughened channel, ASME J. Turbomachinery, Vol. 113, No. 1, pp. 123-130.
DOI
|
7 |
Ahn, S. W., Lee, M. S., Jeong, S. S., and Bae, S. T., 2014, Effect of rib pitch on heat transfer and friction factor in a two wall divergent channel, Korean J. of Air-Cond. & Refri. Eng., Vol. 26, No. 4, pp.175-180(in Korean).
DOI
|
8 |
Lee, M. S. and Ahn, S. W., 2016, Heat transfer friction factors in the ribbed square convergent and divergent channels, Heat and Mass Transfer, Vol. 52, No. 6, pp. 1109-1116.
DOI
|
9 |
Bergman, T. L., Incropera, F. P., and Lavine, A. S., 2011, Fundamentals of Heat and Mass Transfer.
|
10 |
Kline, S. J. and McClintock, F. A., 1953, Describing uncertainties in single-sample experiments, Mechanical Engineering, Vol. 75, pp. 3-8.
|
11 |
Choi, C., Rhee, D. H., and Cho, H. H., 2002, Heat/mass transfer and pressure drop in a square duct with V-shaped ribs, Trans. of KSME(B), Vol. 26, No. 11, pp. 1542-1551(in Korean).
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12 |
Taslim, M. E., Li, T., and Kercher, D. M., 1994, June, Experimental heat transfer and friction in channels roughened with angled, V-shaped and discrete ribs on two opposite walls, In ASME 1994 International Gas Turbine and Aeroengine Congress and Exposition, pp. V004T09A018.
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