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四种风洞收缩段流场特性对比

高丽敏 刘哲 蔡明

高丽敏, 刘哲, 蔡明. 四种风洞收缩段流场特性对比[J]. 航空动力学报, 2020, 35(8): 1695-1705. doi: 10.13224/j.cnki.jasp.2020.08.014
引用本文: 高丽敏, 刘哲, 蔡明. 四种风洞收缩段流场特性对比[J]. 航空动力学报, 2020, 35(8): 1695-1705. doi: 10.13224/j.cnki.jasp.2020.08.014
GAO Limin, LIU Zhe, CAI Ming. Comparison on flow field characteristics of four wind tunnel contraction sections[J]. Journal of Aerospace Power, 2020, 35(8): 1695-1705. doi: 10.13224/j.cnki.jasp.2020.08.014
Citation: GAO Limin, LIU Zhe, CAI Ming. Comparison on flow field characteristics of four wind tunnel contraction sections[J]. Journal of Aerospace Power, 2020, 35(8): 1695-1705. doi: 10.13224/j.cnki.jasp.2020.08.014

四种风洞收缩段流场特性对比

doi: 10.13224/j.cnki.jasp.2020.08.014
基金项目: 国家自然科学基金重大项目(51790512); 民机专项

Comparison on flow field characteristics of four wind tunnel contraction sections

  • 摘要: 基于西北工业大学高亚声速平面叶栅风洞,测量了维氏收缩段的出口流场,发现其方向场品质较差,相比速度场和总压场,核心区沿周向减小了15%。对四种收缩段进行数值模拟后,对比了收缩段的出口核心区、均匀性及分离特性,发现维氏曲线在前部收缩,进口收缩过急引起旋涡,但出口稳流段较长,因此出口均匀性更好。双三次曲线在后部收缩,主流区顺压梯度更大,因此附面层更薄,气流偏角更小,分离特性更好,但出口过冲更大。现有维氏收缩段的三维结构在拓宽核心区同时对气流扰动较大,恶化速度场与方向场,气流偏角增加最大达43%。进口管径对双三次收缩段的流场特性影响不大。

     

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出版历程
  • 收稿日期:  2020-01-08
  • 刊出日期:  2020-08-28

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