Aerodynamic Characteristics Analysis and Ballistic Simulationof Morphing Guided Projectile

JIA Ang;WANG Xugang;LI Guangcai

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    Published By: Journal Of Ballistics

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Journal Of Ballistics ›› 2022, Vol. 34 ›› Issue (04) : 74-82. DOI: 10.12115/j.issn.1004-499X(2022)04-011

Aerodynamic Characteristics Analysis and Ballistic Simulationof Morphing Guided Projectile

  • JIA Ang1,WANG Xugang1,LI Guangcai2
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Abstract

In order to maintain a better aerodynamic shape of the guided projectile in different flight states,improve the flight efficiency and increase the range,a morphing guided projectile was designed. The aerodynamic parameters calculation,aerodynamic characteristics analysis,ballistic simulation were carried out. Firstly,the aerodynamic layout of the morphing guided projectile was determined according to the design parameters,and the specific shape parameters of the wing,canard and tail fin of projectile were determined through iterative optimization,the control modes and ballistic characteristics of the morphing guided projectile were described. Then the aerodynamic data of the morphing guided projectile was calculated by using engineering algorithms,the relationship between lift coefficient,drag coefficient,static stability and the change of the projectile wing shape was analyzed. Finally,a morphing scheme was developed for the designed morphing guided projectile based on the results of aerodynamic characteristics analysis. Hp-adaptive pseudo-spectrum method was used to optimize the ballistics of the morphing guided projectile and the fixed-profile guided projectile with the goal of maximum range. The results show that the designed morphing guided projectile meets the design parameters and has good aerodynamic characteristics and maneuverability,and the ballistic calculation results show that the range can be increased by 10% to 22.5% by introducing the morphing flight technology.

Key words

morphing guided projectile / ballistic optimization / ballistic calculation / variable-sweep wing

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JIA Ang1,WANG Xugang1,LI Guangcai2. Aerodynamic Characteristics Analysis and Ballistic Simulationof Morphing Guided Projectile. Journal Of Ballistics. 2022, 34(04): 74-82 https://doi.org/10.12115/j.issn.1004-499X(2022)04-011

References

[1] 徐云涛. 智能变形飞行器发展及关键技术研究[J]. 战术导弹技术,2017,38(2):26-33.
XU Yuntao. Research on the development and key technology of smart morphing aircraft[J]. Tactical Missile Technology,2017,38(2):26-33.(in Chinese)
[2]孙杨,昌敏,白俊强. 变形机翼飞行器发展综述[J]. 无人系统技术,2021,4(3):65-77.
SUN Yang,CHANG Min,BAI Junqiang,et al. Review of morphing wing aircraft[J]. Unmanned Systems Technology,2021,4(3):65-77.(in Chinese)
[3]白鹏,陈钱,徐国武,等. 智能可变形飞行器关键技术发展现状及展望[J]. 空气动力学学报,2019,37(3):426-443.
BAI Peng,CHEN Qian,XU Guowu,et al. Development status of key technologies and exception about smart morphing aircraft[J]. Acta Aero-dynamica Sinica,2019,37(3):426-443.(in Chinese)
[4]AJAJ R M,BEAVERSTOCK C S,FRISWELLM I. Morphing aircraft:the need for a new design philosophy[J]. Aerospace Science and Technology,2016,49:154-166.
[5]WEISSHAAR T A. Morphing aircraft systems:historical,perspectives and future Challenges[J]. Journal of Aircraft,2013,50(2):337-353.
[6]贺媛媛,王博甲. 国外变形飞行器的研究现状[J]. 飞航导弹,2013,43(10):49-55.
HE Yuanyuan,WANG Bojia. Current status of research on foreign morphing aircraft[J]. Aerodynamic Missile Journal,2013,43(10):49-55.(in Chinese)
[7]冯金富,陈国明,张萌. 变体技术在兵器设计上的应用[J]. 兵器装备工程学报,2017,38(12):215-220.
FENG Jinfu,CEHN Guoming,ZHANG Meng. Application of morphing technology in aircraft[J]. Journal of Ordnance Equipment Engineering,2017,38(12):215-220.(in Chinese)
[8]TAKAHASHI T,SPALL R,TURNER D,et al. A multi-disciplinary survey of advanced subsonic tactical cruise missile configurations[C]//43rd AIAA Aerospace Sciences Meeting and Exhibit. Reno,Nevada,US:AIAA,2005:709.
[9]TAKAHASHI T,SPALL R,TURNER D. A multi-disciplinary assessment of morphing aircraft technology applied to tactical cruise missile configurations[C]//45th AIAA/ASME/ASCE/AHS/ASC Structure,Structural Dynamics & Materials Confer. Palm Springs,California,US:AIAA,2004:1725.
[10]陈战辉,谢军伟,付云. 变体技术在巡航导弹上的应用研究[J]. 飞航导弹,2011,41(8):32-35.
CHEN Zhanhui,XIE Junwei,FU Yun. Study on the application of morphing technology on cruise missiles[J]. Aerodynamic Missile Journal,2011,41(8):32-35.(in Chinese)
[11]韩光松,李萍. 巡航导弹智能变形研究[J]. 舰船电子工程,2019,39(10):62-66.
HAN Guangsong,LI Ping. Study on smart morphing of cruise missiles[J]. Ship Electronic Engineering,2019,39(10):62-66.(in Chinese)
[12]DILLSAVER M,FRANKE M. Wind tunnel study of oblique wing missile model[C]//46th AIAA Aerospace Sciences Meeting and Exhibit. Reno,Nevada,US:AIAA,2008:318.
[13]王明亮,吴威涛,封锋,等. 变掠翼巡航导弹气动特性及最优掠角分析[J]. 兵器装备工程学报,2022,43(7):197-202.
WANG Mingliang,WU Weitao,FENG Feng,et al. Analysis of aerodynamic characteristics and optimal sweep angle of variable swept cruise missile[J]. Journal of Ordnance Equipment Engineering,2022,43(7):197-202.
[14]陈铁彪,王洪波,康永来,等. 变形技术在助推-滑翔飞行器中的应用前景分析[J]. 战术导弹技术,2017,38(5):1-5.
CHEN Tiebiao,WANG Hongbo,KANG Yonglai,et al. Application prospects of morphing technology in the boost-glide vehicle[J]. Tactical Missile Technology,2017,38(5):1-5.(in Chinese)
[15]LI Y,YI L,AO Y,et al. Simulation analysis the aerodynamic characteristics of variable sweep wing missile[J]. Journal of Physics. Conference Series,2020,1570(1):12073.
[16]YI L,LI Y,MA L,et al. Analysis of aerodynamic characteristics of missile with different sweep angle under supersonic condition[J]. Journal of Physics. Conference Series,2021,1802(4):42003.
[17]王旭刚,陈琦,王中原. 远程变后掠翼巡航导弹多任务弹道设计及仿真[J]. 弹道学报,2018,30(3):13-17.
WANG Xugang,CHEN Qi,WANG Zhongyuan. Multi-task trajectory design and simulation for long-range swing-wing cruise missile[J]. Journal of Ballistics,2018,30(3):13-17.(in Chinese)
[18]赵日,孙瑞胜,沈坚平. 变后掠翼制导炸弹滑翔弹道优化设计[J]. 航天控制,2014,32(1):16-20.
ZHAO Ri,SUN Ruisheng,SHEN Jianping. The optimization design of glide trajectory for guide bomb with morphing swept wings[J]. Aerospace Control,2014,32(1):16-20.(in Chinese)
[19]王娜,陈洁卿,明超,等. 基于hp-自适应伪谱法的变后掠翼导弹弹道优化设计[J]. 弹道学报,2016,28(4):24-29.
WANG Na,CHEN Jieqing,MING Chao,et al. Optimization design for trajectory of morphing-wing missile based on hp-adaptive pseudo-spectral method[J]. Journal of Ballistics,2016,28(4):24-29.(in Chinese)

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