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轴对称及二元喷管RCS的数值模拟

杨涛 杨青真 李岳锋

杨涛, 杨青真, 李岳锋. 轴对称及二元喷管RCS的数值模拟[J]. 航空动力学报, 2011, 26(8): 1819-1823.
引用本文: 杨涛, 杨青真, 李岳锋. 轴对称及二元喷管RCS的数值模拟[J]. 航空动力学报, 2011, 26(8): 1819-1823.
YANG Tao, YANG Qing-zhen, LI Yue-feng. Numerical simulation of RCS for axisymmetric nozzles and symmetrical two-dimensional nozzle[J]. Journal of Aerospace Power, 2011, 26(8): 1819-1823.
Citation: YANG Tao, YANG Qing-zhen, LI Yue-feng. Numerical simulation of RCS for axisymmetric nozzles and symmetrical two-dimensional nozzle[J]. Journal of Aerospace Power, 2011, 26(8): 1819-1823.

轴对称及二元喷管RCS的数值模拟

Numerical simulation of RCS for axisymmetric nozzles and symmetrical two-dimensional nozzle

  • 摘要: 利用物理光学迭代法独立设计程序,采用前后向算法并结合欠松弛因子加速收敛,提高运算效率.通过计算简单标准模型的雷达散射截面(RCS)验证了程序的可靠性.在此基础上,对两种不同宽高比二元喷管简化模型及轴对称喷管简化模型的RCS进行了计算并加以分析比较.结果表明,程序具有较好的计算精度和通用性,在较大范围的姿态角内,二元喷管简化模型的RCS高于轴对称喷管简化模型的RCS.

     

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出版历程
  • 收稿日期:  2010-09-15
  • 修回日期:  2011-01-04
  • 刊出日期:  2011-08-28

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