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正癸烷/空气旋转爆轰波形成与传播数值模拟

邵晓峰 赵宁波 刘世铮 孟庆洋 李雅军 郑洪涛

哈尔滨工程大学学报2024,Vol.45Issue(4):730-738,9.
哈尔滨工程大学学报2024,Vol.45Issue(4):730-738,9.DOI:10.11990/jheu.202204003

正癸烷/空气旋转爆轰波形成与传播数值模拟

Numerical simulations of the formation and propagation of an n-decane/air rotating detonation wave

邵晓峰 1赵宁波 1刘世铮 2孟庆洋 1李雅军 2郑洪涛1

作者信息

  • 1. 哈尔滨工程大学 动力与能源工程学院,黑龙江 哈尔滨 150001
  • 2. 中国船舶集团有限公司第七〇三研究所,黑龙江 哈尔滨 150078
  • 折叠

摘要

Abstract

To investigate the formation and propagation of a gas-liquid two-phase rotating detonation wave,three-di-mensional numerical simulations were conducted to discuss the formation and evolution characteristics and self-sus-taining propagation mechanism of n-decane/air rotating detonation wave using the Euler-Lagrangian method.The results reveal that the detonation and pressure waves with different intensities can be obtained by adjusting the ini-tial fuel distribution during the ignition stage.In the collision stage,four collisions occurred between the detonation and pressure waves.Owing to the lack of fuel supply,the pressure wave gradually decayed and disappeared,and the detonation wave propagated in a single-wave mode.In the stable propagation stage,the unburned fuel accumu-lated at the contact triple point to form an unreacted gas flow region and a local explosion was induced.The period-ic occurrence of the unreacted gas flow region and local explosion are important factors affecting the self-sustained propagation of two-phase detonation waves.

关键词

正癸烷/气液两相/非预混/旋转爆轰/掺混/流场特性/自持传播/未反应气流区

Key words

n-decane/gas-liquid two-phase/region/rotating detonation/mixing/flow field characteristics/self-sustaining propagation/unreacted gas flow regio

分类

航空航天

引用本文复制引用

邵晓峰,赵宁波,刘世铮,孟庆洋,李雅军,郑洪涛..正癸烷/空气旋转爆轰波形成与传播数值模拟[J].哈尔滨工程大学学报,2024,45(4):730-738,9.

基金项目

国家自然科学基金项目(52071103). (52071103)

哈尔滨工程大学学报

OA北大核心CSTPCD

1006-7043

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