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Comparative Study of Convective Heat Transfer Performance of Steam and Air Flow in Rib Roughened Channels 被引量:4

Comparative Study of Convective Heat Transfer Performance of Steam and Air Flow in Rib Roughened Channels
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摘要 A comparative experimental study of heat transfer characteristics of steam and air flow in rectangular channels roughened with parallel ribs was conducted by using an infrared camera. Effects of Reynolds numbers and rib angles on the steam and air convective heat transfer have been obtained and compared with each other for the Reynolds number from about 4,000 to 15,000. For all the ribbed channels the rib pitch to height ratio(p/e) is 10, and the rib height to the channel hydraulic diameter ratio is 0.078, while the rib angles are varied from 90° to 45°.Based on experimental results, it can be found that, even though the heat transfer distributions of steam and air flow in the ribbed channels are similar to each other, the steam flow can obtain higher convective heat transfer enhancement capability, and the heat transfer enhancement of both the steam and air becomes greater with the rib angle deceasing from 90° to 45°. At Reynolds number of about 12,000, the area-averaged Nusselt numbers of the steam flow is about 13.9%, 14.2%, 19.9% and 23.9% higher than those of the air flow for the rib angles of 90°,75°, 60° and 45° respectively. With the experimental results the correlations for Nusselt number in terms of Reynolds number and rib angle for the steam and air flow in the ribbed channels were developed respectively. A comparative experimental study of heat transfer characteristics of steam and air flow in rectangular channels roughened with parallel ribs was conducted by using an infrared camera. Effects of Reynolds numbers and rib an-gles on the steam and air convective heat transfer have been obtained and compared with each other for the Rey-nolds number from about 4,000 to 15,000. For all the ribbed channels the rib pitch to height ratio (p/e) is 10, and the rib height to the channel hydraulic diameter ratio is 0.078, while the rib angles are varied from 90° to 45°. Based on experimental results, it can be found that, even though the heat transfer distributions of steam and air flow in the ribbed channels are similar to each other, the steam flow can obtain higher convective heat transfer enhancement capability, and the heat transfer enhancement of both the steam and air becomes greater with the rib angle deceasing from 90° to 45°. At Reynolds number of about 12,000, the area-averaged Nusselt numbers of the steam flow is about 13.9%, 14.2%, 19.9% and 23.9% higher than those of the air flow for the rib angles of 90°, 75°, 60° and 45° respectively. With the experimental results the correlations for Nusselt number in terms of Rey-nolds number and rib angle for the steam and air flow in the ribbed channels were developed respectively.
出处 《Journal of Thermal Science》 SCIE EI CAS CSCD 2018年第2期184-194,共11页 热科学学报(英文版)
基金 funded by the National Natural Science Foundation of China(Funding No.51206109)
关键词 空气流动 肋骨 蒸气 隧道 转移性能 对流 粗糙 学习 steam cooling air cooling rib-roughened channel gas turbine heat transfer
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  • 1Goldstein R J. Film cooling. Advances in Heat Transfer 1971; 7(1): 321-379.
  • 2Moffat R J. Turbine blade cooling. Symposium on Heat Transfer in Rotating Machinery. 1985.
  • 3Metzger D E, Berry R A, Bromson J P. Developing heat transfer in rectangular ducts with staggered arrays of short pin fins. Journal of Heat Transfer 1982; 104(4): 700-706.
  • 4Metzger D E, Haley S W. Heat transfer experiments and flow visualization for arrays of shortpin fins. ASME Paper, 1982-GT-138, 1982.
  • 5Metzger D E, Fan S C, Haley S W. Effects of pin shape and array orientation on heat transfer and pressure loss in pin fin arrays. Journal of Engineering for Gas Turbines and Power 1984; 106(1): 252-257.
  • 6Han J C. Heat transfer and friction in channels with two opposite rib-roughened walls. Journal of Heat Transfer 1984; 106(4): 774-781.
  • 7Han J C, Park J S. Developing heat transfer in rectangular channels with rib turbulators. International Journal of Heat and Mass Transfer 1988; 31(1): 183-195.
  • 8Chupp R E, Helms H E, McFadden P W, et al. Evaluation of internal heat transfer coefficients for impingement cooled turbine airfoils. Journal of Aircraft 1968; 6: 203-208.
  • 9Metzger D E, Bunker R S. Local heat transfer in internally cooled turbine airfoil leading edge regions: Part II—impingement cooling with film coolant extraction. Journal of Turbomachinery 1990; 112(3): 459-466.
  • 10Yanovski L S. Physical basis of transpiration cooling for engines of flying apparatus. Moscow: MAI Press, 1996.

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