亚半球罩形成杆式射流正交设计的数值分析
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国家自然科学基金资助(11572291);山西省研究生联合培养基地人才培养项目资助(20160033)


Numerical Analysis of Orthogonal Design of Rod Shaped Jet with Hemispherical Shroud
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    摘要:

    为研究亚半球罩形成杆式射流的成型因素,利用非线性动力学软件AUTODYN-2D 对其成型过程进行数 值模拟。分析亚半球罩外曲率半径、罩高、壁厚和装药长径比4 种因素对杆式射流头部速度以及头尾速度差的影响 规律,在此基础上对4 种因素影响杆式射流的头部速度和头尾速度差的主次关系进行正交设计研究,并通过数据处 理得到4 种因素各水平的最优组合。研究结果表明:随着装药长径比、亚半球罩外曲率半径、罩高的增大以及亚半 球罩壁厚的减小,杆式射流的头部速度和头尾速度差增大;装药长径比是影响头部速度的主要因素,外曲率半径对 头部速度影响最小;罩高是影响头尾速度差的主要因素,外曲率半径和壁厚对头尾速度差影响较小。该研究可为杆 式射流结构优化提供参考价值。

    Abstract:

    In order to study the forming factors of the rod shaped jet in the hemispherical shroud, the forming process was numerically simulated by nonlinear dynamics software AUTODYN-2D. The analysis of outer radius of curvature, hemisphere cover height, wall thickness and charge length/diameter ratio of the four factors on the velocity of jet head and tail rod speed difference influence of orthogonal design on the basis of research on the influence of four factors of rod like jet head velocity and tail velocity difference between primary and secondary, optimal combination and get through the data processing of every level of four factors. The results show that with the charge ratio of length to diameter, radius of curvature, sub hemisphere hood cover high increase and decrease the sub hemisphere cover thickness of the rod head and tail jet speed difference increases; the charge length / diameter ratio is the main factor affecting the head velocity, radius of outer curvature head speed with minimal impact cover; high is the main factor affecting the head velocity difference, outer curvature radius and wall thickness on the head and tail velocity difference has little effect. The research can provide reference value for structural optimization of rod jet.

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刘亚昆,吴国东,伊建亚.亚半球罩形成杆式射流正交设计的数值分析[J].,2017,36(10).

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  • 收稿日期:2017-06-04
  • 最后修改日期:2017-08-17
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  • 在线发布日期: 2018-11-02
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