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燃气轮机透平叶片气热耦合计算

胡捷 刘建军 江友钿

胡捷, 刘建军, 江友钿. 燃气轮机透平叶片气热耦合计算[J]. 航空动力学报, 2011, 26(2): 349-354.
引用本文: 胡捷, 刘建军, 江友钿. 燃气轮机透平叶片气热耦合计算[J]. 航空动力学报, 2011, 26(2): 349-354.
HU Jie, LIU Jian-jun, JIANG You-dian. Conjugate heat transfer investigation on a gas turbine blade[J]. Journal of Aerospace Power, 2011, 26(2): 349-354.
Citation: HU Jie, LIU Jian-jun, JIANG You-dian. Conjugate heat transfer investigation on a gas turbine blade[J]. Journal of Aerospace Power, 2011, 26(2): 349-354.

燃气轮机透平叶片气热耦合计算

基金项目: 国家重点基础研究发展计划(2007CB210108)

Conjugate heat transfer investigation on a gas turbine blade

  • 摘要: 针对具有热态实验结果的Mark Ⅱ冷却叶片进行气热耦合计算研究,利用CFX求解器对非耦合与耦合算法进行了详细的分析和对比.结果表明,相比耦合计算及实验结果,由于非耦合边界条件的影响,采用施加平均壁面温度的非耦合计算存在较大的计算偏差.研究工作揭示了气热耦合计算的必要性及准确性.

     

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    [9] 董平,黄洪燕,冯国泰.高压燃气涡轮径向内冷叶片气热耦合的数值分析[J].航空动力学报,2008,23(2):201-207. DONG Pin,HUANG Hongyan,FENG Guotai.Conjugate heat transfer analysis of a high pressure turbine vane with radial internal cooling passages[J].Journal of Aerospace Power,2008,23(2):201-207.(in Chinese)
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出版历程
  • 收稿日期:  2009-12-24
  • 修回日期:  2010-04-17
  • 刊出日期:  2011-02-28

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