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Numerical Study of Lateral Jet Interaction for Oblique Jet Powered Missile
Received date: 2015-04-07
Online published: 2025-05-28
Lateral jet interaction for oblique jet powered missile was simulated numerically by solving N-S equations. Through investigating shocks and vortices structure of lateral jet interaction flowfield and oblique jet powered flowfield effects of angle of attack and Mach number on lateral jet flowfield structure and surface pressure coefficient distribution were analyzed, and variation feature of lateral jet interaction effect was studied, the results indicate that jet force is reduced by interaction force when lateral jet at windward side and is amplified when interaction force at leeward side at higher angle of attack, while jet moment is amplified by interaction moment when lateral jet both at windward side and at leeward side.
Key words: missile; lateral jet; numerical simulation; flowfield structure
ZHU Zhonggen , LI Jie , GAO Hongchao . Numerical Study of Lateral Jet Interaction for Oblique Jet Powered Missile[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2015 , 35(5) : 138 -142 . DOI: 10.15892/j.cnki.djzdxb.2015.05.033
| [1] | Brandeis J, Gill J. Experimental investigation of side-jet steering for supersonic and hypersonic missiles[J]. Journal of Spacecraft and Rockets, 1996. 33 (3): 296-302. |
| [2] | Brandeis J, Gill J. Experimental investigation of super-and hypersonic jet interaction on missile configurations[J]. Journal of Spacecraft and Rockets, 1998. 35 (2): 296-302. |
| [3] | Graham MJ, Weinacht P, Brandeis J. Numerical investigation of supersonic jet interaction for axisymmetric bodies[J]. Journal of Spacecraft and Rockets, 2000. 37 (5): 675-683. |
| [4] | Graham MJ, Weinacht P, Brandeis J. Numerical investigation of supersonic jet interaction for finned bodies[J]. Journal of Spacecraft and Rockets, 2002. 39 (3): 376-383. |
| [5] | 唐志共, 杨彦广, 刘君, 等. 横向喷流干扰/控制研究进展 实验流体力学, 2010, 24 (4): 1-6. |
| [6] | 阎超. 计算流体力学方法及应用[M]. 北京: 北京航空航天大学出版社, 2006. |
| [7] | 张涵信, 沈孟育. 计算流体力学: 差分方法的原理和应用[M]. 北京: 国防工业出版社, 2003. |
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