This paper experimentally investigated a transpiration cooling performance of double-laminated and triple-laminated sintered woven wire mesh structures with different porosities and arrangements. Each laminated test piece was made up of two or three layers, and each layer has different porosities and same thickness. The porosities of layers include 25.6%, 37.1%, 46.9%, and 55.1%. All the tests were performed with air. The flow rate and temperature of main flow were kept at 300 kg/hr and 90 °C, respectively. The blowing ratio between the cooling air and main flow approximately varied from 1.2% to 9%. The average surface temperature of test pieces was captured by an infrared thermal imager. The cooling effectiveness for each specimen was calculated and analyzed. Moreover, the pressure drop of several specimens was analyzed with modified Darcy equation. The results showed that the flow behavior agrees well with the modified Darcy equation. The average porosity of the test piece has a great influence on flow behavior, and the air flow direction through a double-laminated porous medium has only slight influence on pressure drop in this study. The results also indicated that the cooling efficiency increases as the average porosity increases. The arrangement of layers affects the transpiration cooling performance, and the cooling efficiency of the laminated model is affected by each laminates together.
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September 2016
Research-Article
An Experimental Investigation on Transpiration Cooling Based on the Multilaminated Sintered Woven Wire Mesh Structures
Jiandong Ma,
Jiandong Ma
National Key Laboratory of Science
and Technology on Aero-Engine
Aero-Thermodynamics,
Collaborative Innovation Center of Advanced
Aero-Engine,
Beihang University,
Beijing 100191, China
and Technology on Aero-Engine
Aero-Thermodynamics,
Collaborative Innovation Center of Advanced
Aero-Engine,
Beihang University,
Beijing 100191, China
Search for other works by this author on:
Xiang Luo,
Xiang Luo
National Key Laboratory of Science
and Technology on Aero-Engine
Aero-Thermodynamics,
Collaborative Innovation Center of Advanced
Aero-Engine,
Beihang University,
Beijing 100191, China
and Technology on Aero-Engine
Aero-Thermodynamics,
Collaborative Innovation Center of Advanced
Aero-Engine,
Beihang University,
Beijing 100191, China
Search for other works by this author on:
Haiwang Li,
Haiwang Li
National Key Laboratory of Science
and Technology on Aero-Engine
Aero-Thermodynamics,
Collaborative Innovation Center of Advanced
Aero-Engine,
Beihang University,
Beijing 100191, China
e-mail: 09620@buaa.edu.cn
and Technology on Aero-Engine
Aero-Thermodynamics,
Collaborative Innovation Center of Advanced
Aero-Engine,
Beihang University,
Beijing 100191, China
e-mail: 09620@buaa.edu.cn
Search for other works by this author on:
Yangpeng Liu
Yangpeng Liu
National Key Laboratory of Science and
Technology on Aero-Engine
Aero-Thermodynamics,
Collaborative Innovation Center of Advanced
Aero-Engine,
Beihang University,
Beijing 100191, China
Technology on Aero-Engine
Aero-Thermodynamics,
Collaborative Innovation Center of Advanced
Aero-Engine,
Beihang University,
Beijing 100191, China
Search for other works by this author on:
Jiandong Ma
National Key Laboratory of Science
and Technology on Aero-Engine
Aero-Thermodynamics,
Collaborative Innovation Center of Advanced
Aero-Engine,
Beihang University,
Beijing 100191, China
and Technology on Aero-Engine
Aero-Thermodynamics,
Collaborative Innovation Center of Advanced
Aero-Engine,
Beihang University,
Beijing 100191, China
Xiang Luo
National Key Laboratory of Science
and Technology on Aero-Engine
Aero-Thermodynamics,
Collaborative Innovation Center of Advanced
Aero-Engine,
Beihang University,
Beijing 100191, China
and Technology on Aero-Engine
Aero-Thermodynamics,
Collaborative Innovation Center of Advanced
Aero-Engine,
Beihang University,
Beijing 100191, China
Haiwang Li
National Key Laboratory of Science
and Technology on Aero-Engine
Aero-Thermodynamics,
Collaborative Innovation Center of Advanced
Aero-Engine,
Beihang University,
Beijing 100191, China
e-mail: 09620@buaa.edu.cn
and Technology on Aero-Engine
Aero-Thermodynamics,
Collaborative Innovation Center of Advanced
Aero-Engine,
Beihang University,
Beijing 100191, China
e-mail: 09620@buaa.edu.cn
Yangpeng Liu
National Key Laboratory of Science and
Technology on Aero-Engine
Aero-Thermodynamics,
Collaborative Innovation Center of Advanced
Aero-Engine,
Beihang University,
Beijing 100191, China
Technology on Aero-Engine
Aero-Thermodynamics,
Collaborative Innovation Center of Advanced
Aero-Engine,
Beihang University,
Beijing 100191, China
1Corresponding author.
Contributed by the Heat Transfer Division of ASME for publication in the JOURNAL OF THERMAL SCIENCE AND ENGINEERING APPLICATIONS. Manuscript received July 10, 2015; final manuscript received November 25, 2015; published online April 12, 2016. Assoc. Editor: Giulio Lorenzini.
J. Thermal Sci. Eng. Appl. Sep 2016, 8(3): 031005 (9 pages)
Published Online: April 12, 2016
Article history
Received:
July 10, 2015
Revised:
November 25, 2015
Citation
Ma, J., Luo, X., Li, H., and Liu, Y. (April 12, 2016). "An Experimental Investigation on Transpiration Cooling Based on the Multilaminated Sintered Woven Wire Mesh Structures." ASME. J. Thermal Sci. Eng. Appl. September 2016; 8(3): 031005. https://doi.org/10.1115/1.4032921
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