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凹面腔尺寸和曲率对激波会聚起爆的影响分析

曾昊 何立明 苏建勇

空气动力学学报2013,Vol.31Issue(1):82-87,93,7.
空气动力学学报2013,Vol.31Issue(1):82-87,93,7.DOI:10.7638/kqdlxxb20130114

凹面腔尺寸和曲率对激波会聚起爆的影响分析

Investigation on the influence of cavity configuration on detonation initiation via shock wave focus

曾昊 1何立明 2苏建勇1

作者信息

  • 1. 空军工程大学工程学院,陕西西安710038
  • 2. 空军西安飞行学院,陕西西安710306
  • 折叠

摘要

Abstract

In order to investigate the influence of cavity configuration on detonation initiation via shock wave focus, detonation initiation with different size cavities and different curvature cavities were simulated, hydrogen-air mixture was used.The results indicate that choosing cavity size should counterpoise both jet intensity and attenuation of incidence shock wave caused by cavity vacuum.Cavity curvature neither too big nor too small.In this article, the performance of portion sphericity cavity with diameter of 74mm is best.

关键词

两级脉冲爆震发动机/爆震波/激波

Key words

two-stage pulse detonation engine/ detonation wave/ shock wave

分类

航空航天

引用本文复制引用

曾昊,何立明,苏建勇..凹面腔尺寸和曲率对激波会聚起爆的影响分析[J].空气动力学学报,2013,31(1):82-87,93,7.

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