ROCKETS TECHNOLOGY

Simulation of Two-dimensional Nozzle with Fluidic Injection for Throat Area Control

  • LI Kun ,
  • WANG Rugen ,
  • GUO Feifei ,
  • HU Jiaguo
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  • Aeronautics and Astronautics Engineering College, Air Force Engineering University, Xi'an 710038, China

Received date: 2014-12-29

  Online published: 2025-05-26

Abstract

In order to analyze the influence of injection total temperature and injection pipe shape on fluid throat area control, numerical simulation was performed on fluid throat control of 2-dimensional convergent-divergent nozzle. Results show that the efficient of throat area control (ETAC) increases gradually along with the increase of injection total temperature; compared the two fluidic nozzles, injection pipe in convergence shape has higher ETAC under lower injection pressure ratio(SPR), while injection pipe in convergence-divergence shape has higher ETAC under higher injection pressure ratio; as SPR increases, ETAC first increases and then decreases; a higher velocity of the injection on injection exit can lead to a higher injection ETAC. Keywords: 2-dimensional nozzle; fluid throat control; injection; numerical simulation

Cite this article

LI Kun , WANG Rugen , GUO Feifei , HU Jiaguo . Simulation of Two-dimensional Nozzle with Fluidic Injection for Throat Area Control[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2015 , 35(3) : 103 -106 . DOI: 10.15892/j.cnki.djzdxb.2015.03.027

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