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含铝凝胶燃料脉冲爆轰发动机工作过程瞬态特性

胡洪波 翁春生

固体火箭技术2016,Vol.39Issue(4):463-469,7.
固体火箭技术2016,Vol.39Issue(4):463-469,7.DOI:10.7673/j.issn.1006-2793.2016.04.003

含铝凝胶燃料脉冲爆轰发动机工作过程瞬态特性

Transient characteristics for working process of pulse detonation engine with aluminized gelled fuels

胡洪波 1翁春生2

作者信息

  • 1. 西安航天动力研究所 液体火箭发动机技术重点实验室,西安 710100
  • 2. 南京理工大学 瞬态物理国家重点实验室,南京 210094
  • 折叠

摘要

Abstract

In order to understand the transient mechanism of pulse detonation engine with gelled fuels during the working process,the mathematical and physical model of pulse detonation engine with aluminized gelled fuels was established.The flow field of a single cycle pulse detonation engine with aluminized gelled fuels was simulated numerically by using the conservation element and solution element method,and the transient characteristics during the detonation reaction and impulse generation processes were analyzed.The calculation results show that the strip of the aluminized gelled fuels droplet under the detonation wave is predominant. The aluminum particles scatter into the detonation tube accompanying with the strip of droplets,and participate in reaction,so the a⁃luminum quantity accumulated in the final stage is small.And the process of the gelled fuels'detonation exhaust can be divided into three typical stages,which are expansion stage attached to detonation,gas"choked" expansion stage and weaken expansion stage in sequence.The results have some significant references for application research on pulse detonation engine with gelled fuels.

关键词

脉冲爆轰发动机/凝胶燃料/爆轰/瞬态/数值计算

Key words

pulse detonation engine/gelled fuels/detonation/transient/numerical calculation

分类

航空航天

引用本文复制引用

胡洪波,翁春生..含铝凝胶燃料脉冲爆轰发动机工作过程瞬态特性[J].固体火箭技术,2016,39(4):463-469,7.

基金项目

国家自然科学基金(11372741)。 ()

固体火箭技术

OA北大核心CSCDCSTPCD

1006-2793

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