Volume 40 Issue 4
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ZHU Jiawei, YANG Xuehe, CHEN Kenlun, et al. Research and application of a novel simulation method for evaluating the traversal chance of flying object through the propeller[J]. Journal of Aerospace Power, 2025, 40(4):20230476 doi: 10.13224/j.cnki.jasp.20230476
Citation: ZHU Jiawei, YANG Xuehe, CHEN Kenlun, et al. Research and application of a novel simulation method for evaluating the traversal chance of flying object through the propeller[J]. Journal of Aerospace Power, 2025, 40(4):20230476 doi: 10.13224/j.cnki.jasp.20230476

Research and application of a novel simulation method for evaluating the traversal chance of flying object through the propeller

doi: 10.13224/j.cnki.jasp.20230476
  • Received Date: 2023-07-24
    Available Online: 2024-08-22
  • Chance quantitative analysis of foreign object crossing through the propeller is difficult due to the complexity of propeller shape and foreign object flight attitude, and there is lack of effective technical means for it. A technical method to analyze the chance of cylindrical foreign object crossing the propeller under multiple engineering applications was presented, such as realistic three-dimensional propeller shape and adjustable foreign object flight attitude, etc. The accuracy of the technical method was verified by comparing the difference between the theoretical and simulated chance of foreign object crossing the rectangular blade propeller. Finally, a certain type propeller was selected to carry out the traversal chance simulation. The results showed that, the technical method presented herein had high analytical accuracy, the maximum absolute error and relative error between traversal chance results of simulation and theoretical calculation under ideal model were 0.92% and 1.10%. Respectively, the traversal chance variation trend of a certain type propeller was consistent with the rectangular blade propeller. Under the same impact conditions of foreign object, traversal chance decreased with the increase of aspect ratio and increased with the increase of impact attitude angle.

     

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