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BALLISIIC AND AIRDYNAMICS

Numerical Study of Lateral Jet Interaction for Oblique Jet Powered Missile

  • ZHU Zhonggen ,
  • LI Jie ,
  • GAO Hongchao
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  • 1 School of Aeronautics, Northwestern Polytechnical University, Xi'an 710072, China
    2 No. 203 Research Institute of China Ordnance Industries, Xi'an 710065, China

Received date: 2015-04-07

  Online published: 2025-05-28

Abstract

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.

Cite this article

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

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Outlines

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