[an error occurred while processing this directive] [an error occurred while processing this directive]
[an error occurred while processing this directive]|
陈麒齐(1996—),女,贵州毕节人,硕士研究生,研究方向:燃气射流相关的计算流体力学。 |
收稿日期: 2021-01-02
网络出版日期: 2025-02-13
Research on the Optimization of Gas Deflector Structure Based on Neural Network
Received date: 2021-01-02
Online published: 2025-02-13
为优化燃气导流器表面热环境,对某型车载单面导流器的热环境影响因素进行数值计算分析,确定了导流器高度、导流器折转半径和导流器背板与发射架距离为重要结构参数,它们与导流器表面温度之间存在复杂非线性关系。基于BP神经网络和RBF径向基神经网络建立相应代理模型进行对比,选择了决定系数更高、稳定性更好的RBF径向基神经网络代理模型进行导流器型面优化,并对优化结果进行了流场计算分析,结果表明,在满足导流器机动性要求的前提下,优化后的导流器表面最大温度降低了约400 K,热环境得到了明显改善,且导流效果更佳。优化误差在1% 之内,验证了优化的有效性和准确性,为今后燃气导流器型面的设计及优化提供了参考。
陈麒齐 , 姜毅 , 王志浩 , 贾启明 . 基于神经网络的燃气导流器型面优化研究[J]. 弹箭与制导学报, 2021 , 41(4) : 103 -107 . DOI: 10.15892/j.cnki.djzdxb.2021.04.023
To optimize the thermal environment of gas deflector,the thermal environment influencing factors of avehicle-mounted single-sided deflector are analyzed by numerical calculation,which proves that the height of the deflector, the turning radiusof the deflector and the distance from the deflector backplane to the launch frame are important parameters, having complex nonlinear relationship with the surface temperature of deflector.Based on the comparison of BP surrogate mathematic model and RBF surrogate mathematic model,the RBF surrogate mathematic model with higher determination coefficient and better stability is selected to optimize the deflector. The flow field numerical calculation of optimization results is carried out,which shows that, on the premise of meeting the maneuverability requirements, the optimized max surface temperature of the deflector is reduced by about 400 K, the thermal environment is significantly improved and the diversion effect is better.The optimization error is within 1%, verified the effectiveness and accuracy of the optimization, which provides a reference for the design and optimization of the gas deflector in the future.
| [1] |
盛文成. 燃气导流器的流动特性数值分析[D]. 南京: 南京理工大学, 2011.
|
| [2] |
刘念昆. 车载导弹垂直发射装置燃气排导的数值研究[D]. 哈尔滨: 哈尔滨工业大学, 2015.
|
| [3] |
李荣. 火炮关键参数误差方案的区间优化及神经网络优选[D]. 南京: 南京理工大学, 2017.
|
| [4] |
赵承庆, 姜毅. 气体射流动力学[M]. 北京: 北京理工大学出版社, 1998:30-35.
|
| [5] |
|
| [6] |
|
| [7] |
李国勇, 杨丽娟. 神经·模糊·预测控制及其MATLAB实现[M]. 3版. 北京: 电子工业出版社, 2013:27-31.
|
| [8] |
马艳丽, 姜毅, 郝继光, 等. 固体发动机燃气射流对发射平台冲击效应研究[J]. 固体火箭技术, 2010, 33(4):373-376.
|
| [9] |
杨风波, 马大为, 任杰, 等. 新型同心筒自力发射热环境优化设计[J]. 固体火箭技术, 2015, 38(2):172-178.
|
| [10] |
刘永, 李淑娟, 李言, 等. 基于中心复合设计试验的SiC单晶片超声振动加工工艺参数优化[J]. 机械工程学报, 2013, 49(7):193-198.
|
| [11] |
王永菲, 王成国. 响应面法的理论与应用[J]. 中央民族大学学报(自然科学版), 2005, 14(3):236-240.
|
| [12] |
苏美娟. 径向基函数神经网络学习算法研究[D]. 苏州: 苏州大学, 2007.
|
| [13] |
公茂果, 焦李成, 杨咚咚, 等. 进化多目标优化算法研究[J]. 软件学报, 2009, 20(2):271-289.
|
/
| 〈 |
|
〉 |