跨介质飞行器头部外形优化及入水性能分析

doi:10.12382/bgxb.2021.0538

摘要/Abstract

摘要： 跨介质飞行器头部外形是影响跨介质过程中运动学特性的重要因素之一。通过采用常见的双参数立方多项式曲线方程，获取跨介质飞行器头部外形曲线无量纲参数，采用任意拉格朗日-欧拉方法完成不同头部外形跨介质飞行器的流固耦合建模及性能分析，研究不同头部外形入水后末速度与入水过程中所受最大冲击应力。以最大末速度和最小冲击应力为优化目标，在保证有限元仿真精度的同时，通过径向基神经网络提升计算效率，并利用多岛遗传算法对跨介质飞行器头部外形进行多目标优化，以得到最佳的头部外形。研究结果表明，跨介质飞行器最优头部外形相对于基本外形，入水过程速度衰减量与所受冲击应力明显降低，有效地减少入水过程中跨介质飞行器的能量损失，可为跨介质飞行器的头部外形设计提供参考。

关键词: 跨介质飞行器, 流固耦合, 头部外形优化设计, 入水性能分析

Abstract: The head shape of a trans-medium aircraft is one of the important factors affecting the kinematics in the trans-medium process. The common two-parameter cubic polynomial curve is used to obtain the shape curve dimensionless parameters of the trans-medium aircraft head shape. The Arbitrary Lagrangian-Eulerian method is adopted to complete the fluid-structure coupling modeling and performance analysis for trans-medium aircraft with different head shapes, and investigate the terminal velocity of different head shapes after entering the water and the maximum impact stress received during the water entry process. Taking the maximum terminal velocity and the minimum impact stress as the optimization goals, multi-objective optimization is carried out on the head shape of the trans-medium aircraft, and an optimal head shape is obtained. The results show that the optimal head shape of the trans-medium aircraft has significantly reduced speed attenuation and impact stress compared with the basic shape, the optimal head shape of the trans-medium aircraft effectively reduces the energy loss of the aircraft in the water-entry process. It can provide insights into the head shape design of the trans-medium aircraft.

Key words: trans-mediumaircraft, fluid-structurecoupling, optimizationdesignofheadshape, waterentryperformanceanalysis

中图分类号:

马文朝，孟繁敏，马诺，孟军辉，邹汝平. 跨介质飞行器头部外形优化及入水性能分析[J]. 兵工学报, 2022, 43(10): 2588-2597.

MA Wenchao, MENG Fanmin, MA Nuo, MENG Junhui, ZOU Ruping. Head Shape Optimization and Water Entry Performance Analysis of Trans-medium Aircraft[J]. Acta Armamentarii, 2022, 43(10): 2588-2597.

参考文献

［1］高英杰, 孙铁志, 张桂勇, 等. 回转体高速倾斜入水的流场特性及结构响应[J]. 爆炸与冲击, 2020, 40(12):101-113.
GAO Y J, SUN T Z, ZHANG G Y, et al. Flow characteristics and structure response of high-speed oblique water-entry for a revolution body[J]. Explosion and Shock Waves, 2020, 40(12): 101-113. (in Chinese)
[2] 王浩宇, 李木易, 程少华, 等. 航行体高速入水问题研究综述[J]. 宇航总体技术, 2021, 5(3):65-70.
WANG H Y, LI M Y, CHENG S H, et al.Review of vehicle's high-speed water entry[J]. Astronautical Systems Engineering Technology, 2021, 5(3):65-70. (in Chinese)
[3] MAY A. Vertical entry of missiles into water[J]. Journal of Applied Physics, 1952, 23(12):1362-1372.
[4] BODILY K G, CARLSON S J, TRUSCOTT T T.The water entry of slender axisymmetric bodies[J]. Physics of Fluids, 2014, 26(7): 45-78.
[5] 张伟, 郭子涛, 肖新科, 等. 弹体高速入水特性试验研究[J]. 爆炸与冲击, 2011, 31(6):579-584.
ZHANG W, GUO Z T, XIAO X K,et al. Experimental investigations on behaviorsof projectile high-speed water entry[J]. Explosion and Shock Waves, 2011, 31(6): 579-584. (in Chinese)
[6] 罗驭川, 黄振贵, 高建国, 等. 截锥体头部外形弹丸低速斜入水试验研究[J]. 爆炸与冲击, 2019, 39(11):80-87.
LUO Y C, HUANG Z G, GAO J G, et al. Experiment research of low-speed oblique water-entryof truncated cone-shaped projectile[J]. Explosion and Shock Waves, 2019, 39(11): 80-87. (in Chinese)
[7] 施红辉, 胡青青, 陈波, 等. 钝体倾斜和垂直冲击入水时引起的超空泡流动特性试验研究[J]. 爆炸与冲击, 2015, 35(5): 617-624.
SHI H H, HU Q Q, CHEN B, et al. Experimental study of supercavitating flows induced by obliqueand vertical water entry of blunt bodies[J]. Explosion and Shock Waves, 2015, 35(5): 617- 624. (in Chinese)
[8] SHI Y, PAN G, YIM S C, et al. Numerical investigation of hydroelastic water-entry impact dynamics of AUVs[J]. Journal of Fluids and Structures, 2019, 91:102760.
[9] 卜广志, 张宇文. 使用多学科设计优化方法对鱼雷总体综合设计的建模思路研究[J].兵工学报, 2005, 26(2):163-168.
BU G Z, ZHANG Y W.Study on models of torpedo synthetic conceptual design with MDO[J].Acta Armamentarii,2005, 26(2): 163-168. (in Chinese)
[10] 宋保维, 李福新. 回转体最小阻力外形优化设计[J]. 水动力学研究与进展(A辑), 1994, 9(5):523-530.
SONG B W, LI F X.Optimum shaping design of axisymmetric bodies for minimum drag[J]. Chinese Journal of Hydrodynamics,1994, 9(5):523-530. (in Chinese)
[11] 李福新, 段培贤, 张宇文. 低噪声回转体头部线型设计[J]. 声学学报, 2002, 27(3):258-262.
LI F X, DUAN P X, ZHANG Y W. Fore-body shaping design of an axisymmetric body for minimum noise[J]. Acta Acustica, 2002, 27(3):258-262. (in Chinese)
[12] 余德海, 宋保维, 杨世兴,等.鱼雷外形多目标多学科综合优化设计方法研究[J].兵工学报, 2008, 29(3):337-340.
YU D H, SONG B W, YANG S X, et al. Investigation of integrated multi-disciplinary and multi-objective optimization of the torpedo shape design method[J]. Acta Armamentarii, 2008, 29(3):337-340. (in Chinese)
[13] 赵加鹏, 张云海, 任翀. 鱼雷外形低阻、低噪和高机动性的多学科优化设计方法[J]. 兵工学报, 2012, 33(2):186-191.
ZHAO J P, ZHANG Y H, REN C. Thetorpedo shape multidisciplinary design optimization methods for low-drag，low-noise and high-maneuverability[J]. Acta Armamentarii, 2012, 33(2):186-191. (in Chinese)
[14] 权晓波, 王惠, 魏海鹏, 等. 基于代理模型的水下航行体头部外形优化设计方法研究[J]. 船舶力学, 2016, 20(10): 1262-1268.
QUAN X B, WANG H, WEI H P, et al. Configuration optimization design of underwater vehicle based on surrogate model[J]. Journal of Ship Mechanics, 2016, 20(10): 1262-1268. (in Chinese)
[15] LUO W L, GUO X M, DAI J W, et al. Hull optimization of an underwater vehicle based on dynamic surrogate model[J]. Ocean Engineering, 2021, 230(1):109050.
[16] 叶鹏程, 王聪聪, 潘光. 基于代理模型的翼身融合水下滑翔机外形优化设计[J].西北工业大学学报, 2021, 39(1):85-92.
YE P C, WANG C C, PAN G. Surrogate based blended-wing-body underwater glider shape optimization design[J]. Journal of Northwestern Polytechnical University, 2021,39(1):85-92. (in Chinese)
[17] 宋盼盼, 赵捍东, 吴建萍. 基于LS-DYNA的弹体入水动力学仿真研究[J].机电技术, 2013(5):18-20.
SONG P P, ZHAO H D,WU J P. Research on dynamics simulation of projectile entering water based on LS-DYNA[J]. Mechanical & Electrical Technology, 2013(5): 18-20. (in Chinese)
[18] 宋盼盼. 三维弹性体入水动力学数值仿真研究[D].太原：中北大学, 2014.
SONG P P. The research on numerical simulation about water entry of 3D elastic body[D].Taiyuan：North University of China,2014. (in Chinese)
[19] 汪振, 吴茂林, 孙玉松, 等.基于多介质ALE算法的柱体高速垂直入水仿真[J].水下无人系统学报, 2020, 28(1):81-88.
WANG Z, WU M L, SUN Y S, et al. Multi-medium ALE algorithm-based simulation of vertical and high-speed water entry of cylinder[J]. Journalof Unmanned Undersea Systems, 2020, 28(1): 81-88. (in Chinese)
[20] 张明. 回转体入水冲击运动响应数值仿真与半理论公式预报研究[D].哈尔滨：哈尔滨工程大学,2018.
ZHANG M.Investigation on numerical simulation and semi-theoritical formula prediction of rotary structure water entry impact motion response[D].Harbin:Harbin Engineering University, 2018. (in Chinese)
[21] 徐思博. 回转体高速入水瞬态流固耦合载荷与弹道特性研究[D].哈尔滨：哈尔滨工程大学, 2019.
XU S B.Study on fluid-structure interactional load and trajectory characteristics of high-speed water entry of projectile[D].Harbin:Harbin Engineering University, 2019.(in Chinese)
[22] 龙腾, 郭晓松, 彭磊, 等. 基于信赖域的动态径向基函数代理模型优化策略[J]. 机械工程学报, 2014, 50(7):184-190.
LONG T, GUO X S, PENG L, et al. Optimization strategy using dynamic radial basis function metamodel based on trust region[J]. Journal of Mechanical Engineering, 2014, 50(7):184-190. (in Chinese)
[23] 韩军, 段荣鑫, 张磊, 等. 基于多岛遗传算法的薄壁齿圈装夹变形优化研究[J]. 机电工程, 2020,37(6):96-100，110.
HAN J, DUAN R X, ZHANG L, et al. Optimization of thin-walled ring gear clamping deformation based on multi-island genetic algorithm[J]. Journal of Mechanical ＆ Electrical Engineering, 2020,37(6):96-100,110. (in Chinese)
[24] AN X Y, CHEN Y, HUANG H C. Parametric design and optimization of the profile of autonomous underwater helicopter based on NURBS[J].Journal of Marine Science and Engineering, 2021, 9(6):668.

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[2]	刘玉标，刘维玮，程载斌，梁乃刚. 通过缩比试验数据计算潜射导弹的载荷[J]. 兵工学报, 2012, 33(8): 916-920.
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[6]	毕小平，蒋陆德，李贺佳. 液力变矩器叶片流固耦合强度分析[J]. 兵工学报, 2008, 29(10): 1158-1162.
[7]	项昌乐，焦开河，王文平，刘辉. 箱体结构动强度的流固耦合有限元分析[J]. 兵工学报, 2007, 28(7): 769-773.
[8]	刘群，姜毅，郝继光. 某型导弹发动机推进剂恶劣エ况下温度仿真研究[J]. 兵工学报, 2007, 28(12): 1463-1467.