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离散孔板气膜冷却对流换热系数的计算 被引量:3

Calculation of Heat Transfer Coefficients of Discrete Hole Board Film Cooling
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摘要 通过对几种不同的气膜冷却对流换热系数的计算方法的归纳总结,提出用相对气膜冷却换热系数的方法来计算气膜冷却时的对流换热.在对6种不同开口规律的离散孔平板进行了实验研究的基础上,用热平衡法建立了离散孔板气膜冷却对流换热模型,用最小二乘法拟合了相应的关系式及关系曲线,并分析了来流参数及离散孔板的孔径、开口率等几何参数对气膜冷却对流换热系数的影响. By analyzing the methods of calculating different heat transfer coefficients,the film cooling relative heat transfer coefficients was used to calculate the heat transfer.After six different discrete hole board being experimented,the model of heat transfer of discrete hole board film cooling was established.The effects on the film cooling heat transfer coefficients of the gas parameters of the flow and the geometric parameters of the discrete hole board were analyzed,and the transfer coefficients were obtained.Some useful conclusions such as the effects of the percent of the discrete hole area to the transfer coefficients were obtained.
出处 《吉首大学学报(自然科学版)》 CAS 2002年第4期35-39,共5页 Journal of Jishou University(Natural Sciences Edition)
基金 国家博士后基金资助项目(2302143724)
关键词 离散孔板 气膜冷却 对流换热系数 热平衡法 计算方法 壁面冷却 discrete hole board film cooling heat transfer wall cooling
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参考文献3

  • 1李锋.高温升大热负荷加力燃烧室壁面冷却结构研究[R].南京:南京航空航天大学博士后研究工作报告,1996.
  • 2ANDREWS G E. Full Coverage Discrete Hole Wall Cooling:Cooling Effectiveness[R]. 84 - GT - 212, ASME.
  • 3ANDREWS G E. Full Coverage Discrete Hole Wall Cooling: The Influence of the Number of Holes and Pressure koss[ R]. 90 - GT -61, ASME.

同被引文献21

  • 1常国强,常海萍,常飞,胡晓东,单学庆.多孔纵向波纹表面气膜冷却效率实验研究[J].航空动力学报,2009,24(3):513-518. 被引量:11
  • 2金捷,马继华,金如山.燃烧室室壁冲击/气膜复合冷却壁温分布研究(二)理论部分[J].推进技术,1994,15(2):34-40. 被引量:7
  • 3韩振兴,朱谷君,冀守礼,龙迎天.气膜冷却燃烧室火焰筒二维壁温分布计算[J].航空动力学报,1995,10(1):83-86. 被引量:13
  • 4Hasan Nasir,Srinath V.Ekkad,Sumanta Acharya.Effect of compound angle injection on flat surface film cooling with large streamwise injection angle[J].Experimental Thermal and Fluid Science,2001(25):23-29.
  • 5宋双文,杨卫华,胡好生,张靖周.冲击+逆向对流+气膜冷却传热特性的研究[J].航空动力学报,2007,22(9):1417-1422. 被引量:17
  • 6Kiran H Dellimore,Carlos Cruz,Andre W Marshall. A jet model for slot film cooling with effect of variation in the mainstream pressure.AIAA-2007-2004[R].2007.
  • 7Taslim M E,Spring S D,Mehlman B P. An experimental investigation of film cooling effectiveness for slots of various exit geometries[J].Journal of Thermophysics and Heat T ransfer,1992.302-307.
  • 8James G Lucas,Richard L Golladay. An experimental in-vestigation of gaseous film cooling of a rocket motor.,NASA TN D-1988[R].1988.
  • 9Carlos A Cruz,Andre W Marshall,Arnaud Trouve. Large-eddy simulation of film cooling through a 2D slot AIAA-2006-4710[R].2006.
  • 10Fernando Raffan,Carlos A Cruz,Kiran Dellimore. Near wall measurements along a film cooled wall .AIAA-2006-4709[R].2006.

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