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Author:

Nianhui YE (Nianhui YE.) | Teng LONG (Teng LONG.) | Junhui MENG (Junhui MENG.) | Renhe SHI (Renhe SHI.) | Baoshou ZHANG (Baoshou ZHANG.)

Abstract:

As a crucial weapon in the sea battle,anti-ship missiles generally employ a sea-skimming penetration strategy to reduce the probability of being detected by the target radar,which greatly increases the risk of touching water caused by sensor errors or random sea conditions.To alleviate the large impact load by high-velocity water touching,a novel anti-ship missile body configuration is proposed in this paper,which is inspired by the idea of hydroplaning.A parametric geometry model is first developed to modify the configuration of the anti-ship missile body.Subsequently,a structured arbitrary Lagrange-Eulerian based Fluid-Structure Interaction(FSI)model is estab-lished to analyze the kinematics parameters of the missile body during the hydroplaning process.A missile body configuration optimization problem is then formulated to minimize the impact load considering several constraints,e.g.,horizontal velocity loss,pitch angle after touching water,and inside capacity for payload.Due to the time-consuming FSI simulation,a Kriging-assisted con-strained differential evolution method is utilized to optimize the missile body configuration for reducing the impact load.During the optimization process,radial basis function and Kriging are combined with evolutionary operators to lead the search to the vicinity of the optimum rapidly.The result shows that the proposed missile body configuration can reduce the impact load by 18.8%compared with the ordinary configuration.Additionally,the optimized configuration can further yield a 17.4%impact load decrease subject to all the constraints and avoid structural dam-age by the high-velocity water touching,which demonstrates the effectiveness and practicability of the proposed anti-ship missile body configuration and corresponding optimization framework for reducing the impact load.

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Author Community:

  • [ 1 ] [Baoshou ZHANG]北京工业大学
  • [ 2 ] [Renhe SHI]北京工业大学
  • [ 3 ] [Nianhui YE]北京工业大学
  • [ 4 ] [Teng LONG]北京工业大学
  • [ 5 ] [Junhui MENG]北京工业大学

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Source :

中国航空学报(英文版)

ISSN: 1000-9361

Year: 2023

Issue: 12

Volume: 36

Page: 268-281

5 . 7 0 0

JCR@2022

Cited Count:

WoS CC Cited Count:

SCOPUS Cited Count:

ESI Highly Cited Papers on the List: 0 Unfold All

WanFang Cited Count: -1

Chinese Cited Count:

30 Days PV: 10

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