Numerical study on the influences of pin-fin diameter on the flow resistance and heat transfer of leaning vent hole lamilloy
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Numerical study on the influences of pin-fin diameter on the flow resistance and heat transfer of leaning vent hole lamilloy
Vol. 22, Issue 4, (2007)
作者机构:
北京航空航天大学 能源与动力工程学院 航空发动机气动热力重点实验室,北京,100083
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Published:2007
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TAO Zhi, L Dong, DING Shui-ting, et al. Numerical study on the influences of pin-fin diameter on the flow resistance and heat transfer of leaning vent hole lamilloy[J]. 2007, 22(4).
DOI:
TAO Zhi, L Dong, DING Shui-ting, et al. Numerical study on the influences of pin-fin diameter on the flow resistance and heat transfer of leaning vent hole lamilloy[J]. 2007, 22(4).DOI:
Numerical study on the influences of pin-fin diameter on the flow resistance and heat transfer of leaning vent hole lamilloy
The influence of pin-fins diameter of minimum elements in the leaning vent hole lamilloy upon the flow resistance and heat transfer was studied through numerical simulation.A locally increased grid density was applied to the bigger area of flow angle with the help of unstructured grid method.k-ε model equation was used to resolve the steady lamilloy along with fixed wall function.The coupling heat transfer was calculated using fluid area and solid area coupling solution.The calculated results were presented
helping to analyze the flow and heat transfer.The research results show that
proper increase of pin-fins diameter is helpful to decrease the flow resistance and increase the cooling efficiency.
Experimental investigation of heat transfer and flow resistance in a crossed-rib channel
Effect of the shape of divider wall on heat transfer and flow resistance characteristic of passage
Heat transfer characteristics of axi-symmetrical nozzle and RS nozzle
Heat transfer characteristics of expander cycle thrust chamber
Experimental investigations on the local heat transfer coefficient of rotating single circular impingement in a half-limited space
Related Author
QIN Ling
DENG Hong-wu
LIN Yu-zhen
LI Li
XU Guo-qiang
DING Shui-ting
DENG Hong-wu
HAN Fei
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 Energy and Mechanical Engineering, North China Electric Power University
School of Astronautics, Beijing University of Aeronautics and Astronautics
College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics