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跨声速HTA涡轮导向器全三维流场计算分析
引用本文:张剑,曾军,程信华,康湧.跨声速HTA涡轮导向器全三维流场计算分析[J].燃气涡轮试验与研究,2003,16(4):21-24.
作者姓名:张剑  曾军  程信华  康湧
作者单位:中国燃气涡轮研究院,成都,610500
摘    要:利用CFD软件CFX-TASCflow对具有试验数据的跨声速HTA涡轮导向器流场进行了计算,结果表明,计算的叶面等熵马赫数分布和出口气流角与试验值吻合良好;而计算的总压恢复系数与试验数据存在一定的差别。

关 键 词:涡轮导向器  三维流场  计算  HTA涡轮  跨声速流动  N-S方程
文章编号:1627-2620(2003)04-0021-04
修稿时间:2003年3月5日

Three-dimensional Flow Field Analysis of the Stator in Transonic HTA Turbine
ZHANG Jian,ZENG Jun,CHENG Xin - hua,KANG Yong.Three-dimensional Flow Field Analysis of the Stator in Transonic HTA Turbine[J].Gas Turbine Experiment and Research,2003,16(4):21-24.
Authors:ZHANG Jian  ZENG Jun  CHENG Xin - hua  KANG Yong
Abstract:Three-dimensional flow fields of transonic HTA turbine stator were calculated using CFD software CFX-TASCflow.The calculated results indicate that the distributions of calculated isentropic Mach number and outlet flow angle agree well with the experimental data,however calculated total pressure recovery coeffi-cient has still some difference.
Keywords:turbine stator  N-S equations  flow field analysis  
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