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融合空间迭代与深度学习的气膜叠加模型

刘星 楼健 余鸿乾 汪奇 杨力 饶宇 刘宇阳

刘星, 楼健, 余鸿乾, 等. 融合空间迭代与深度学习的气膜叠加模型[J]. 航空动力学报, 2025, 40(2):20230134 doi: 10.13224/j.cnki.jasp.20230134
引用本文: 刘星, 楼健, 余鸿乾, 等. 融合空间迭代与深度学习的气膜叠加模型[J]. 航空动力学报, 2025, 40(2):20230134 doi: 10.13224/j.cnki.jasp.20230134
LIU Xing, LOU Jian, YU Hongqian, et al. A film superposition model integrating spatial iteration and deep learning[J]. Journal of Aerospace Power, 2025, 40(2):20230134 doi: 10.13224/j.cnki.jasp.20230134
Citation: LIU Xing, LOU Jian, YU Hongqian, et al. A film superposition model integrating spatial iteration and deep learning[J]. Journal of Aerospace Power, 2025, 40(2):20230134 doi: 10.13224/j.cnki.jasp.20230134

融合空间迭代与深度学习的气膜叠加模型

doi: 10.13224/j.cnki.jasp.20230134
基金项目: 中国空气动力研究与发展中心结冰与防除冰重点实验室开放课题资助(2201IADL20220403)
详细信息
    作者简介:

    刘星(1998-),男,硕士生,主要从事燃气轮机涡轮叶片气膜冷却研究。E-mail:zslxbh@sjtu.edu.cn

  • 中图分类号: V233.1

A film superposition model integrating spatial iteration and deep learning

  • 摘要:

    结合神经网络方法发展一套隐含物理变量的空间迭代算法用于气膜叠加模型,并通过全覆盖气膜平板综合冷效实验和绝热数值模拟分别进行验证,解决了直接采用神经网络方法不蕴含真实物理规律以及缺乏可解释性的问题。通过精度对比和隐含变量挖掘,获得垂直平板方向5倍平板前缘边界层厚度位置处沿侧向的速度等4个可解释的气膜叠加模型关键封闭变量,验证了融合模型的精度和可靠性。

     

  • 图 1  全覆盖气膜冷却实验台示意图

    Figure 1.  Schematic of experimental device of fully coverage film cooling

    图 2  全覆盖气膜冷却实验台实物图

    Figure 2.  Photo of experimental device of fully coverage film cooling

    图 3  数值模拟计算域

    Figure 3.  Computational field of numerical simulation

    图 4  Sellers 叠加模型

    Figure 4.  Sellers superposition model

    图 5  平板上方计算域

    Figure 5.  Computational field above the plate

    图 6  迭代算子网络架构

    Figure 6.  Framework of the physically iterative arithmetic convolution network

    图 7  随机孔板训练集结果(综合冷效实验数据)

    Figure 7.  Results of random orifice plate training set (based on experimental data of comprehensive cooling efficiency)

    图 8  随机孔板测试集结果(综合冷效实验数据)

    Figure 8.  Results of random orifice plate test set (based on experimental data of comprehensive cooling efficiency)

    图 9  随机孔板训练集结果(绝热冷效数值模拟数据)

    Figure 9.  Results of random orifice plate training set (based on numerical simulation data of adiabatic cooling efficiency)

    图 10  随机孔板测试集结果(绝热冷效数值模拟数据)

    Figure 10.  Results of random orifice plate test set (based on numerical simulation data of adiabatic cooling efficiency)

    图 11  全覆盖气膜冷却近壁面变量分布

    Figure 11.  Near wall parameters distribution of fully coverage film cooling

    图 12  迭代算子全覆盖气膜叠加模型隐含层

    Figure 12.  Hidden state of fully coverage film superposition model

    图 13  隐含层与参数的回归关系

    Figure 13.  Regression relationship between hidden state and parameters

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出版历程
  • 收稿日期:  2023-03-07
  • 网络出版日期:  2024-08-29

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