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弯曲进气道内外二维湍流流场数值分析与实验研究
引用本文:翁培奋,郭荣伟.弯曲进气道内外二维湍流流场数值分析与实验研究[J].上海大学学报(自然科学版),1995,1(5):490-498.
作者姓名:翁培奋  郭荣伟
作者单位:上海市应用数学和力学研究所,南京航空航天大学动力工程系
基金项目:国家自然科学基金,上海市高校青年教师学术基金
摘    要:本文应用有限体积法以二个埋入式弯曲进气管道内外流场进行了数值分析计算,其中用TTM法生成了较为合理贴体曲线坐标网格,用k-ε双方程形式湍流模型近似地模化了进气道内外的复杂湍流流声援笔有关实验数据对照后表明:来自进气道前方的进气气流一部分被管道吸入,另一部分沿着机体表面方向流过,管道进气口背风侧处存在一个明显分离区,进气道内部气流流动已经出现了严重畸变,数值计算和有关实验数据吻合得较好,为进一步研究

关 键 词:进气道  湍流  流场  数值分析  航空发动机

Investigation of Two-dimensional Separated Flow in and around a Submerged Curved Intake
Weng Peifen,Zhou Zhewei.Investigation of Two-dimensional Separated Flow in and around a Submerged Curved Intake[J].Journal of Shanghai University(Natural Science),1995,1(5):490-498.
Authors:Weng Peifen  Zhou Zhewei
Institution:Weng Peifen;Zhou Zhewei(Shanghai Institute of Appl. Math. and Mech.)Guo Rongwei (Nanjing University of Aeronautics & Astronautics)
Abstract:This paper presents investigation of two dimensional separated flow in and around a submerged curved intake by experiment and computation. The NavierStokes equations are employed which are discreted in body-fitted coordinate system by finite control volume method. The results show that the flow separation near and behind the inlet exists and the duct flow is distorted.Comparison between the calculation and experimental data is fairly satisfactory.
Keywords:inlet  flow distortion  separated flow  numerical analysis
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