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Numerical simulation on improving film cooling effectiveness with crescent-shaped block plasma actuator
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College of Aeronautics and Astronautics Engineering, Air Force Engineering University,College of Aeronautics and Astronautics Engineering, Air Force Engineering University,College of Aeronautics and Astronautics Engineering, Air Force Engineering University,College of Aeronautics and Astronautics Engineering, Air Force Engineering University,College of Aeronautics and Astronautics Engineering, Air Force Engineering University

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V231.1

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    Abstract:

    Numerical simulation was carried out to investigate the film cooling mechanism of the crescent-shaped block & plasma actuator structure. With CFD method, flow field characteristics, temperature characteristics and cooling effectiveness were analyzed for different film cooling structures: the common circle-hole, crescent-shaped block and plasma actuator film cooling structure. The results show that in circle-hole film cooling structure, counter-rotating vortex pair(CRVP), which lifted the cooling flow and entrain the hot flow, was formed, therefore the cooling effectiveness was the lowest. In the plasma actuator structures and crescent-shaped block structures, anti-CRVP, which restrained the scale and strength of CRVP, was formed. Compared to that with common circle-hole cooling structure, the film cooling effectiveness is improved a lot both in lateral and streamwise. In the crescent-shaped block & plasma actuator structure, the anti-CRVP reached its maximum, therefore significantly improving cooling effectiveness in the area between the holes and generating the best cooling performance.

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ZHAO Zi-chen, HE Li-ming, ZHANG Qian, XIAO Yang, DAI Shen-ji. Numerical simulation on improving film cooling effectiveness with crescent-shaped block plasma actuator[J]. Advances in Aeronautical Science and Engineering,2016,7(2):135-142

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History
  • Received:January 02,2016
  • Revised:February 05,2016
  • Adopted:March 11,2016
  • Online: June 21,2016
  • Published: