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多循环脉冲爆震发动机爆震室内部压力分布实验研究

陈景彬 郑龙席 黄希桥 卢杰 陈星谷

实验流体力学2013,Vol.27Issue(3):41-46,6.
实验流体力学2013,Vol.27Issue(3):41-46,6.

多循环脉冲爆震发动机爆震室内部压力分布实验研究

Experimental studies on the internal pressure distribution in the detonation combustor of multi-cycle pulse detonation engine

陈景彬 1郑龙席 1黄希桥 1卢杰 1陈星谷1

作者信息

  • 1. 西北工业大学动力与能源学院,西安710072
  • 折叠

摘要

Abstract

Based on the multi-cycle air-breathing pulse detonation engine experiments,realtime pressure data from 9 positions along the detonation combustor axial have been obtained.After analysis of the data from time domain and frequency domain,curved surfaces of pressure with axial location and time of a cycle working in 6 frequencies have been fitted by using MATLAB software GRIDDATA function.Analyzing the fitted data from different perspectives,we find that using DDT initiation will generate a local high-pressure region before the detonation wave,after the detonation wave generation the average speed of detonation wave maintained at about 1000m/s,and its peak pressure and randomness increase.The experimental conclusions provide a foundation to study the structure and strength of the detonation combustor.

关键词

脉冲爆震发动机/多循环/爆震室/内部压力

Key words

pulse detonation engine/ multi-cycle/detonation combustor/internal pressure

分类

航空航天

引用本文复制引用

陈景彬,郑龙席,黄希桥,卢杰,陈星谷..多循环脉冲爆震发动机爆震室内部压力分布实验研究[J].实验流体力学,2013,27(3):41-46,6.

实验流体力学

OA北大核心CSCDCSTPCD

1672-9897

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