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相关技术

燃气发生器绝热层烧蚀数值仿真

  • 周源 ,
  • 齐强 ,
  • 陈志刚 ,
  • 徐明
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  • 1 海军航空工程学院, 山东 烟台 264001
    2 91515部队, 海南 三亚 572000

周源(1979-), 男, 安徽濉溪人, 讲师, 博士研究生, 研究方向:兵器发射理论与技术.

收稿日期: 2014-03-14

  网络出版日期: 2025-05-26

基金资助

国家自然科学基金(51005242)

Numerical Simulation for Ablation of Insulator in Gas-generator

  • ZHOU Yuan ,
  • QI Qiang ,
  • CHEN Zhigang ,
  • XU Ming
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  • 1 Naval Aeronautical and Astronautical University, Shandong Yantai 264001, China
    2 No. 91515 Unit, Hainan Sanya 572000, China

Received date: 2014-03-14

  Online published: 2025-05-26

摘要

为了研究燃气发生器燃烧室绝热层的传热烧蚀过程,建立了热化学烧蚀计算模型和绝热层传热计算模型。考虑到烧蚀过程中绝热层边界的移动,根据预测—校正格式对模型进行离散,并采用拟牛顿法对绝热层的烧蚀过程及传热过程进行了耦合计算。计算得到了绝热层表面温度、烧蚀率和烧蚀厚度等参数的变化规律。计算结果表明,预测—校正格式和拟牛顿法可以用于求解时动边界的瞬态传热模型。

本文引用格式

周源 , 齐强 , 陈志刚 , 徐明 . 燃气发生器绝热层烧蚀数值仿真[J]. 弹箭与制导学报, 2015 , 35(2) : 141 -144 . DOI: 10.15892/j.cnki.djzdxb.2015.02.036

Abstract

In order to study thermal behavior and ablation of insulator in the combustor of gas-generator, the thermo-chemistry ablation model and heat transfer calculation model were established. Considering the fact that the boundary of insulator is moving during the ablation, the models were discredited with predicted-correction method. Coupling calculations were carried out for insulator ablation and temperature field with quasi-Newton method. Temperature of inner wall, ablation velocity and ablation thickness were calculated. The results show that the predicted-correction method and the quasi-Newton method can be applied in unsteady heat transfer and ablation problem with moving boundary.

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参考文献

[1]
徐善玮, 侯晓, 张宏安. 固体火箭发动机内绝热层烧蚀质量损失计算[J]. 固体火箭技术, 2003, 26(3):28-31.
[2]
张涛, 孙冰. 三维烧蚀内部热响应数值计算研究[J]. 宇航学报, 2012, 33(3): 298-304.
[3]
李宛珊, 王文洽. 二维热传导方程的有限差分区域分解算法[J]. 山东大学学报:理学版, 2011, 46(12): 1-5.
[4]
冯立伟. 热传导方程几种差分格式的MATLAB 数值解法比较[J]. 沈阳化工大学学报, 2011, 25(2): 179-182.
[5]
张雪艳, 周爱霞. 时动边界上热传导问题的求解方法[J]. 廊坊师范学院学报:自然科学版, 2010, 10(2): 9-12.
[6]
张斌, 刘宇, 王长辉, 等. 长时间工作固体火箭发动机燃烧室热防护层烧蚀计算[J]. 固体火箭技术, 2011, 34(2): 189-192.
[7]
杨春杰. 固体火箭发动机后效冲量研究[D]. 长沙: 国防科技大学, 2011.
[8]
南京大学数学系计算数学专业. 偏微分方程数值解法[M]. 北京: 科学出版社, 1979: 145-182.
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