Volume 21 Issue 6
Dec.  2006
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YANG Wei-hua, MA Guo-feng, ZHANG Jing-zhou. Experimental study on convective heat transfer characteristics of film cooling with tab[J]. Journal of Aerospace Power, 2006, 21(6): 978-983.
Citation: YANG Wei-hua, MA Guo-feng, ZHANG Jing-zhou. Experimental study on convective heat transfer characteristics of film cooling with tab[J]. Journal of Aerospace Power, 2006, 21(6): 978-983.

Experimental study on convective heat transfer characteristics of film cooling with tab

  • Received Date: 2005-11-15
  • Rev Recd Date: 2006-02-22
  • Publish Date: 2006-12-28
  • In order to study the effect of tab on film cooling,three kinds of test pieces with different geometrical parameters were designed,and the heat transfer characteristics of them were experimentally studied.The results show that the convective heat transfer coefficient of film cooling with tab is better than that without the tab.While the area ratio is 0.1,the convective heat transfer coefficient of film cooling is the best at the blow ratio of 0.50.78;while the area ratio is 0.27,the convective heat transfer coefficient gets its maximum value at the blow ratio of 1.221.5.However,because of the existence of tabs,the flow friction loss in the film hole will be increased.

     

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  • [1]
    葛绍岩,刘登瀛,徐靖中,等.气膜冷却[M].北京:科学出版社,1985.
    [2]
    Rhee Dong Ho,Lee Youn Seok,Kim Young Bonq,et al.Film cooling and thermal field measurements for staggered rows of rectangular-shaped film cooling holes[M].ASME,International Gas Turbine Institute,Turbo Expo (Publication) IGTI,2003,5:423-432.
    [3]
    Ronqquanq Jia,Sunden Benqt,Miron Petetre,et al.Numerical and experimental study of the slot film cooling jet with various angles[A].Proceedings of the ASME Summer Heat Transfer Conference[C],2003,pp:845-856.
    [4]
    Bradbury L J,Khadem A H.The distortion of a jet by tabs[J].Journal of Fluid Mechnics,1975,70(4):801-813.
    [5]
    Zaman K B M Q.Reduction of jet penetration in a cross-flow by using tabs[R].AIAA Paper 98-3276.
    [6]
    Zaman K B M Q.Effect of oscillating tabs on a jet-in-cross-flow[R].AIAA Paper 2003-0632.
    [7]
    Gritsch M,Schulz A,Witting S.Effect of crossflows on the discharge coefficient of film cooling holes with varying angles of inclination and orientation[J].Journal of Turbomachinery,2001,123(4):781-787.
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