大攻角侧向多喷干扰流场特性数值模拟

doi:10.7527/S1000-6893.2015.0054

Abstract

Abstract:

The influence of the interaction flow field with multi-lateral jets on the aerodynamic characteristics of one missile at high angles of attack is investigated using computational fluid dynamics (CFD) method. The CFD method based on Reynolds-averaged Navier-Stokes (RANS) equations is first validated using a standard model with lateral jet and a missile of high fineness ratio, and the capability of solving jet interaction flow field and flow field around a missile at high angles of attack is confirmed. Numerical simulations are then performed on the interaction flow field with multi-lateral jets at high angles of attack. The results show that the angle of attack and the number of lateral jets have a relatively large influence on the aerodynamic load distribution. The differences in the axial distribution of the normal force coefficient and the flow structure between jet-on and jet-off reveal the mechanism of the jet interaction effects on the aerodynamic characteristics of the missile at different angles of attack. Preliminary analysis of the influence of the lateral jets on the pull-up maneuver is provided in the end and the results show that the lateral jets cannot speed up the pull-up process at an altitude of 10 km.

Key words: missile, high angle of attack, lateral jets, aerodynamic characteristics, computational fluid dynamics

CLC Number:

V211.3

LI Bin, WANG Xuezhan, LIU Xianming. Numerical investigation of multi-lateral jets interactions flow characteristics at high angle of attack[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2015, 36(9): 2828-2839.

References

[1] Fan H T. Characteristics and key technologies of the fifth generation of air to air missiles[J]. Aeronautical Science & Technology, 2011(3): 1-5 (in Chinese). 樊会涛. 第五代空空导弹的特点及关键技术[J]. 航空科学技术, 2011(3): 1-5.
[2] Srivastava B. Aerodynamic performance of supersonic missile body and wingtip mounted lateral jets[J]. Journal of Spacecraft and Rockets, 1998, 35(3): 278-286.
[3] Margason R J. Fifty years of jet in cross flow research, AGARD-CP-534[R]. Paris: AGARD, 1993.
[4] Roger R P. The aerodynamics of jet thruster control for supersonic/hypersonic endo-interceptors: Lessons learned, AIAA-1999-0804[R]. Reston: AIAA, 1999.
[5] Tang Z G, Yang Y G, Liu J, et al. The investigation and expectation on lateral jet interaction/control[J]. Journal of Experiments in Fluid Mechanics, 2010, 24(4): 1-6 (in Chinese). 唐志共, 杨彦广, 刘君, 等. 横向喷流干扰/控制研究进展[J]. 实验流体力学, 2010, 24(4): 1-6.
[6] Li S X. Progress in aerodynamics of combination control for vehicles at high speed[J]. Advances in Mechanics, 2009, 39(6): 740-755 (in Chinese). 李素循. 近空间飞行器的气动复合控制原理及研究进展[J]. 力学进展, 2009, 39(6): 740-755.
[7] Graham M J, Weinacht P. Numerical investigation of supersonic jet interaction for axi-symmetric bodies[J]. Journal of Spacecraft and Rockets, 2000, 37(5): 675-683.
[8] Graham M J, Weinacht P, Brandeis J. Numerical investigation of supersonic jet interaction for finned bodies[J]. Journal of Spacecraft and Rockets, 2002, 39(3): 376-383.
[9] Wang S J. Numerical simulation for interaction flow field between external and lateral jet flow[D]. Beijing: Beijing Institute of Technology, 2008 (in Chinese). 王树军. 旋转导弹横向喷流干扰流场数值模拟[D]. 北京: 北京理工大学, 2008.
[10] Byung Y M, Jae W L, Yung H B. Investigation of the shock interaction effect on the lateral jet controlled missile, AIAA-2003-3932[R]. Reston: AIAA, 2003.
[11] Zhou W, Liu H, Liu J, et al. Numerical simulation of lateral jet interaction in supersonic flow[J]. Acta Aeronautica et Astronautica Sinica, 2004, 25(2): 108-112 (in Chinese). 周维, 刘宏, 刘嘉, 等. 超声速来流中侧向喷流干扰流场的数值模拟[J]. 航空学报, 2004, 25(2): 108-112.
[12] Sun D C, Wang G, Jia X H, et al. Influence of double jet on air-to-air missile with lateral injection control[J]. Journal of Solid Rocket Technology, 2007, 30(3): 188-190 (in Chinese). 孙德川, 王广, 贾晓洪, 等. 双喷流对空空导弹直接力控制的影响[J]. 固体火箭技术, 2007, 30(3): 188-190.
[13] Ma M S, Deng Y Q, Zheng M, et al. Numerical investigation of supersonic jet interactions for tactical bodies[J]. Acta Aerodynamic Sinica, 2007, 25(4): 468-473 (in Chinese). 马明生, 邓有奇, 郑鸣, 等. 超声速侧向多喷流干扰特性数值模拟[J]. 空气动力学学报, 2007, 25(4): 468-473.
[14] Ebrahimi H B. Numerical investigation of jet interaction in a supersonic freestream[J]. Journal of Spacecraft and Rockets, 2008, 45(1): 95-103.
[15] Liu X Q, Wu Y Z. The computation of the lateral jet turbulence flow using DES method[J]. Acta Aeronautica et Astronautica Sinica, 2004, 25(3): 209-213 (in Chinese). 刘学强, 伍贻兆. 用DES数值模拟具有横向喷流的稳流流场[J]. 航空学报, 2004, 25(3): 209-213.
[16] Xu Y, Xu X, Wang Z J, et al. Experimental investigation on multi-jet interference[J]. Journal of Experiments in Fluid Mechanics, 2012, 26(5): 13-16 (in Chinese). 徐筠, 徐翔, 王志坚, 等. 多喷口喷流对侧向喷流流场影响的风洞试验研究[J]. 实验流体力学, 2012, 26(5): 13-16.
[17] Sekar B. Three dimensional computation of parallel and non-parallel injection in supersonic flow, AIAA-1995-0886 [R]. Reston: AIAA, 1995.
[18] Chen J Q, Zhang Y F, Jiang D W, et al. Numerical simulation of complex flow with multi lateral jets interactions[J]. Chinese Journal of Theoretical and Applied Mechanics, 2008, 40(6): 735-743 (in Chinese). 陈坚强, 张毅锋, 江定武, 等. 侧向多喷口干扰复杂流动数值模拟研究[J]. 力学学报, 2008, 40(6): 735-743.
[19] Wang J Q, Li S X. Study on the characteristics of interaction flow fields induced by supersonic multi-jets[J]. Chinese Journal of Theoretical and Applied Mechanics, 2009, 41(4): 575-583 (in Chinese). 王军旗, 李素偱. 超声速多喷流干扰流场特性研究[J]. 力学学报, 2009, 41(4): 575-583.
[20] Aswin G, Chakraborty D. Numerical simulation of transverse side jet interaction with supersonic free stream[J]. Aerospace Science and Technology, 2010, 14(5): 295-301.
[21] Li L P, Xu M. Character and effect of interaction between a lateral jet and supersonic cross-flow at large angles of attack[J]. Journal of Solid Rocket Technology, 2011, 34(5): 543-547 (in Chinese). 李立沛, 徐敏. 大攻角侧向喷流流场特性及喷流干扰效应[J]. 固体火箭技术, 2011, 34(5): 543-547.
[22] Li J, Li B, Liu X M, et al. The effect of jet interaction on aerodynamic characteristic at high angle of attack for missile[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2013, 33(4): 153-156 (in Chinese). 李剑, 李斌, 刘仙名, 等. 侧向喷流对导弹大攻角气动特性影响数值研究[J]. 弹箭与制导学报, 2013, 33(4): 153-156.
[23] Anderson J D. Computational fluid dynamics: Basic and application[M]. Wu S P, Zhao L M, translated. Beijing: China Machine Press, 2007: 57-65 (in Chinese). Anderson J D. 计算流体力学: 基础与应用[M]. 吴颂平, 赵刘淼, 译. 北京: 机械工业出版社, 2007: 57-65.
[24] Menter F R. Two-equation eddy-viscosity turbulence mmodels for engineering applications[J]. AIAA Journal, 1994, 32(8): 1598-1605.
[25] Fan H T. Air-to-air missile conceptual design[M]. Beijing: Aviation Industry Press, 2013: 49-50 (in Chinese). 樊会涛. 空空导弹方案设计原理[M]. 北京: 航空工业出版社, 2013: 49-50.
[26] Brandeis J, Gill J. Experimental investigation of supersonic and hypersonic jet interaction on missile configurations[J]. Journal of Spacecraft and Rockets, 1998, 35(3): 296-302.
[27] Голуоев И С. Anti-aircraft missile design[M]. Beijing: China Astronautic Publishing House, 2004: 210-211 (in Chinese). 戈卢别夫 И С. 防空导弹设计[M]. 北京: 中国宇航出版社, 2004: 210-211.

Numerical investigation of multi-lateral jets interactions flow characteristics at high angle of attack

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 15

Recommended Articles

Metrics

Comments

[1]	Qi LIU, Yongjie SHI, Zhiyuan HU, Guohua XU. Parameter effects analysis on aerodynamic and aeroacoustic characteristics of coaxial rigid rotor [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(9): 528856-528856.
[2]	Dazhi SUN, Xi CHEN, Weicheng BAO, Wei BIAN, Qijun ZHAO. Interferences of high-speed helicopter fuselage on aerodynamic and aeroacoustic source characteristics of propeller [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(9): 529142-529142.
[3]	Hongmiao ZHOU, Jianqiao YU, Yong YU. Dynamic modeling and bifurcation analysis of agile turn of parafoil⁃missile system [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(7): 229012-229012.
[4]	Yurou DAI, Jian LI, Xiaopeng XUE, Wei RONG. Aerodynamic characteristics of supersonic disk-gap-band parachute with different reefing ways [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(7): 128811-128811.
[5]	Fengxia LU, Kun WEI, Chunlei WANG, Heyun BAO, Rupeng ZHU. Accessibility of metal particles in three-phase flow of helicopter intermediate gearbox [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(1): 128524-128524.
[6]	Yunchong ZHU, Yangang LIANG, Kebo LI, Yuanhe LIU. Task assignment algorithm for intelligent missile swarm based on PSO and RRT [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(S1): 727354-727354.
[7]	Jiong REN, Gang WANG, Guodong HU, Xiaolu SHI. Adaptive finite volume method with Walsh basis functions [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(8): 127444-127444.
[8]	Siyuan CHANG, Yao XIAO, Guangli LI, Zhongwei TIAN, Kaikai ZHANG, Kai CUI. Effect of wing dihedral and anhedral angles on hypersonic aerodynamic characteristics of high-pressure capturing wing configuration [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(8): 127349-127349.
[9]	Zheng LI, Jianqiao YU, Xinyun ZHAO. Fixed⁃time convergent sliding mode control for agile turn of air⁃to⁃air missiles [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(8): 327262-327262.
[10]	Yuanhe LIU, Kebo LI, Shaoming HE, Yangang LIANG. Flying range control guidance for varying⁃speed missiles based on optimal error dynamics [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(7): 326909-326909.
[11]	Wenbo CAO, Yilang LIU, Weiwei ZHANG. Accelerated convergence method for fluid dynamics solvers based on reduced⁃order model and gradient optimization [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(6): 127090-127090.
[12]	Lei HE, Weiqi QIAN, Kangsheng DONG, Xian YI, Congcong CHAI. Aerodynamic characteristics modeling of iced airfoil based on convolution neural networks [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(5): 126434-126434.
[13]	Wenlong BAO, He JIA, Xiaopeng XUE, Xuejiao HUANG, Shuyi GAO, Wei RONG, Qi WANG, Zhuangzhi WU. Influence of ‘windows’ structure on inflation process of ringsail parachute [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(5): 226936-226936.
[14]	Yiting TAN, Wuxing JING, Changsheng GAO, Ruoming AN. Multiple constrained analytical capture region for hypersonic maneuvering target interception [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(22): 328436-328436.
[15]	Yuxiang FAN, Rui ZHAO, Zhengxuan ZUO, Guang YANG, Yu LI. Gas⁃injection effects on wall heat flux and skin⁃friction of vehicles [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(21): 528587-528587.