MISSILES AND GUIDANCE TECHNOLOGY

Performance Test and Research of Some Non-valve Pulsejet Engine

  • CHEN Gang ,
  • LI Xiaozhu ,
  • LIU Jianguo ,
  • LIU Shujie
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  • No. 203 Research Institute of China Ordnance Industries,Xi’an 710065,China

Received date: 2013-04-09

  Online published: 2025-05-26

Abstract

Ground experiment of the non-valve pulsejet engine was finished. The thrust data and pressure data of the engine were measured and analyzed. The high frequency work principle and process of the pulsejet engine were researched combined with the pressure data. Be directed against the characteristic of the thrust data,digital simulation was done,which proved that the direct thrust test could cause amplitude modulation. Direct thrust test was deficient,and two kinds of improved measure were brought forward.

Cite this article

CHEN Gang , LI Xiaozhu , LIU Jianguo , LIU Shujie . Performance Test and Research of Some Non-valve Pulsejet Engine[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2013 , 33(6) : 106 -109 . DOI: 10.15892/j.cnki.djzdxb.2013.06.011

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