Heat transfer investigation of the channels with 90° rib turbulators and double-row bleed holes
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Heat transfer investigation of the channels with 90° rib turbulators and double-row bleed holes
Vol. 25, Issue 10, (2010)
作者机构:
西北工业大学 动力与能源学院,西安,710072
作者简介:
基金信息:
DOI:
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Published:2010
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GUO Tao, ZHU Hui-ren, XU Du-chun. Heat transfer investigation of the channels with 90° rib turbulators and double-row bleed holes[J]. 2010, 25(10).
DOI:
GUO Tao, ZHU Hui-ren, XU Du-chun. Heat transfer investigation of the channels with 90° rib turbulators and double-row bleed holes[J]. 2010, 25(10).DOI:
Heat transfer investigation of the channels with 90° rib turbulators and double-row bleed holes
The detailed heat transfer distributions of the wall with bleed holes in a channel with 90° rib turbulators and double-row bleed holes were measured by using transient liquid crystal technique.The effects of the relative positions of rib turbulators and bleed holes
channel Reynolds numbers and bleed ratios on heat transfer characteristics were studied.The results show that:the heat transfer distributions are affected by the combined effect of the flow separation
reattachment and bleeding;the heat transfer characteristics for the bleed holes near the upstream ribs are best because of the heat transfer improvement in backflow region and heat transfer enhancement in reattachment region by bleed effect.For the case of the bleed holes near the downstream ribs
the heat transfer characteristics turn worse since higher heat transfer regions behind the holes are confined by ribs;the change of bleed hole location do not modify the position of the flow reattachment
but affect the heat transfer distribution and intensity in the region;the average heat transfer enhancement decreases with the growing Reynolds number
and slightly increases with the increase of bleed ratio.
Experimental investigation on effect of small auxiliary holes on film cooling effectiveness
Heat transfer measurements of turn-over channel in turbine blade
Experiment of impingement heat transfer with film holes bleeding and side bleeding
Experiment of the effects of geometrical parameters on internalheat transfer in an impinging contraction channel with liquid crystal transient technique
Experimental research on film cooling characteristics of cylindrical hole and expanding hole on the leading edge
Related Author
LUO Xiang
TAO Zhi
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ZHU Hui-ren
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WANG Xiao-zeng
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Related Institution
National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics,School of Jet Propulsion, Beijing University of Aeronautics and Astronautics
School of Power and Energy, Northwestern Polytechnical University