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Journal of Projectiles, Rockets, Missiles and Guidance >

2010 , Vol. 30 >Issue 5: 153 - 155

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2010.05.018

BALLISTIC AND AIRDYNAMICS

Numerical Simulation of Slender Body with Supersonic Lateral Jet

  • YANG Tanshu ,
  • LI Bin
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  • 1 Luoyang Institute of Science and Technology, Henan Luoyang 471023, China
    2 China Airborne Missile Academy, Henan Luoyang 471009, China

Received date: 2009-11-23

  Online published: 2025-05-28

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Abstract

The lateral jet interaction in supersonic flow was simulated numerically by solving Navier-Stokes equations with CFD solver. The AUSMDV scheme was adopted to deal with the governing equations. The vortex and wave structures were studied and the topology of separation flow was given according to the CFD results. The CFD results agree well with experiment values.

Key words： jet interaction; computational fluid dynamic; AUSMDV scheme

Cite this article

YANG Tanshu , LI Bin . Numerical Simulation of Slender Body with Supersonic Lateral Jet[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2010 , 30(5) : 153 -155 . DOI: 10.15892/j.cnki.djzdxb.2010.05.018

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