Experiment on heat exchange and cooling of pulse detonation engine detonation tube wall

Xi Qiao Huang, Yang Li, Yue Fei Xiong, Yuan Yuan 1yuan, Long Xi Zheng

科研成果: 期刊稿件文章同行评审

1 引用 (Scopus)

摘要

Experimental investigation for pulse detonation engine (PDE) tube wall temperature distribution along axial direction with or without cooling water using Pt100 thermal resistance was conducted. The results indicate that the outer detonation tube wall temperature increases as the engine's detonation frequency increases at the same axial location of detonation tube. At the same detonation frequency, the outer detonation tube wall temperature in the zone far away from the thrust wall is higher than that in the zone near the thrust wall. The outer detonation tube wall temperature and the temperature gradient reduces when the cooling water is filled into the detonation heat exchange system. The temperature of outer detonation tube wall could be decreased by 106.5℃ when the PDE works for 16 s at the detonation frequency of 20 Hz.

源语言英语
页(从-至)2817-2823
页数7
期刊Hangkong Dongli Xuebao/Journal of Aerospace Power
29
12
DOI
出版状态已出版 - 1 12月 2014

指纹

探究 'Experiment on heat exchange and cooling of pulse detonation engine detonation tube wall' 的科研主题。它们共同构成独一无二的指纹。

引用此