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Experimental Studies on Cooling Effectiveness of the Double-Decker Air Jet Impingement With Film Outflow

[+] Author Affiliations
Junkui Mao, Zhenxiong Liu

Nanjing University of Aeronautics and Astronautics, Nanjing, Jiangsu, China

Wen Guo, Jun Zeng

China Gas Turbine Establishment, Chengdu, Sichuan, China

Paper No. GT2007-27299, pp. 295-304; 10 pages
doi:10.1115/GT2007-27299
From:
  • ASME Turbo Expo 2007: Power for Land, Sea, and Air
  • Volume 4: Turbo Expo 2007, Parts A and B
  • Montreal, Canada, May 14–17, 2007
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 0-7918-4793-4 | eISBN: 0-7918-3796-3
  • Copyright © 2007 by ASME

abstract

Experiments were carried out to investigate the cooling effectiveness of a lamellar double-decker impingement/effusion structure. Infrared radiation (I.R.) thermal camera was used to measure the temperature on the outside surface of the lamellar double-decker. Experimental results were obtained for a wide range of governing parameters (blowing rate M (0.0017∼0.0066), the ratio of the jet impingement distance to the diameter of film hole H/D (0.5∼1.25), the ratio of the distance between the jet hole and film hole to the diameter of the film hole P/D (0, 3, 4), and the material of double-decker (Steel and Copper)). It was observed that the local cooling effectiveness η varies with all these parameters in a complicated way. All the results show that higher cooling effectiveness η is achieved in larger blowing rate cases. A certain range of H/D and P/D can be designed to result in the maximum cooling effectiveness η. And η is less sensitive to the material type compared with those parameters such as H/D, M and P/D.

Copyright © 2007 by ASME
Topics: Cooling , Air jets , Outflow

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