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涡轮叶片外换热计算程序对比研究
引用本文:卿雄杰,潘炳华,曾军.涡轮叶片外换热计算程序对比研究[J].航空动力学报,2010,25(4):741-747.
作者姓名:卿雄杰  潘炳华  曾军
作者单位:中国航空工业集团公司,中国燃气涡轮研究院,成都,610500
摘    要:对两种涡轮叶片外换热计算程序STAN 5和S1ICH的数值方法进行了比较.采用STAN5和S1ICH程序完成了VKI(Von Karman Institute)高压涡轮导叶和动叶叶栅的外传热系数计算,并将计算结果与试验数据进行了对比.结果表明,S1ICH预估的转捩位置、外传热系数的精度较高,同时S1ICH具有适应性广,收敛性好,准备初始参数方便的特点,满足工程设计计算的要求.

关 键 词:涡轮叶片  外传热系数  转捩  湍流模型
收稿时间:3/25/2009 9:10:33 AM
修稿时间:3/7/2010 11:03:27 PM

Comparison of external heat transfer codes for turbine blades
QING Xiong-jie,PAN Bing-hua and ZENG Jun.Comparison of external heat transfer codes for turbine blades[J].Journal of Aerospace Power,2010,25(4):741-747.
Authors:QING Xiong-jie  PAN Bing-hua and ZENG Jun
Institution:china gas turbine establishment,china gas turbine establishment,china gas turbine establishment
Abstract:Comparison for the mathematical models of two external heat transfer (EHT) codes, STAN5 and S1ICH, was done. Both codes were employed to calculate the EHT coefficients (EHTC) of two turbine blades, calling Von Karman Institute(VKI) high-pressure turbine guide vane and blade, and the results were compared with experimental data, which shows that S1ICH has higher precision on capturing onset of transition, and higher precision on predicting EHTC of turbine blades than STAN5. S1ICH can meet the requirement of engineering applications, which has the character of extensive applicability, good convergence and simple input.
Keywords:turbine blades  external heat transfer coefficients (EHTC)  transition  turbulence model
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