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纹影流动显示技术在超音速射流数值模拟验证中的应用

Application of schlieren photograph visualization for validating the numerical simulation method of supersonic jet flow

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【作者】 杨京龙何枫谢峻石许宏庆

【Author】 YANG Jingbng, HE Feng, XU Hongqing(Dep. of Eng. Mech., Tsinghua University, Beijing 100084)

【机构】 清华大学工程力学系

【摘要】 为了研究总压探针测量方法在欠膨胀超音速射流中的可行性,论文采用非结构网格有限体积法对含探针和不含探针的射流流场进行数值模拟,并通过对两个计算结果的比较,给出这种测量方法的参考性评价。为了证明数值方法及计算结果的可靠性,给出了相同条件下纹影流场显示和总压探针测量等实验结果。

【Abstract】 In this paper a numerical analysis method of estimating the total pressure measure error has been developed by means of comparison between the numerical simulation of underexpanded supersonic jet flow with a total pressure probe and that without total pressure probe. Schlieren photograph visualization and total pressure measurement were carried out for validating the feasibility of this numerical analysis method. As a example, the estimation of total pressure measure error has been given at pressure ratio 4:1 under the size condition of φ1.3 mm and φ6mm of total pressure probe outside diameter and nozzle exit inside diameter respectively. This method also can be applied to estimate total pressure measure error in other supersonic flow.

【基金】 清华大学-SMC株式会社国际合作项目
  • 【会议录名称】 流动显示’2002第五届全国流动显示学术会议论文集
  • 【会议名称】流动显示’2002第五届全国流动显示学术会议
  • 【会议时间】2002-07
  • 【会议地点】中国烟台
  • 【分类号】O354.3
  • 【主办单位】中国空气动力学会、中国力学学会
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