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Journal of Projectiles, Rockets, Missiles and Guidance >

2021 , Vol. 41 >Issue 4: 113 - 119

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2021.04.025

Analysis and Simulation of Ramjet in Future Long-range Air-to-air Missile

  • ZHENG Xuyang ,
  • LIU Chang ,
  • LIU Saihua
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  • China Airborne Missile Academy, Henan Luoyang 471009, China

Received date: 2021-01-14

  Online published: 2025-02-13

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Abstract

According to the current development trend of air-to-air missile, the tactical characteristics of the fifth generation air-to-air missile based on ramjet are analyzed, and the air-to-air missile mission (air-to-air combat and ground attack) is given. With reference to “meteor” air-to-air missile, considering the basic characteristics of small size, long-range and high-speed of future embedded long-range air-to-air missile, the calculation model of ramjet is established with two-dimensional three wave system inlet, side intake cavity combustor and axisymmetric Laval nozzle. The three-dimensional three wave ramjet (small size, diameter 167 mm) at high Mach number (3.0~5.0) is completed. The feasibility of the ramjet as an embedded long-range high-speed air-to-air missile in the future is preliminarily verified by dimensional numerical calculation and analysis.

Key words： air to air missile; ramjet; embedded long-range high-speed; three-dimensional numerical simulation; whole engine calculation; aeroengine

Cite this article

ZHENG Xuyang , LIU Chang , LIU Saihua . Analysis and Simulation of Ramjet in Future Long-range Air-to-air Missile[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2021 , 41(4) : 113 -119 . DOI: 10.15892/j.cnki.djzdxb.2021.04.025

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