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Study on Acoustic Detection of the Working State of Pulse Detonation Engine.

Authors :
Zhu, Yan-fang
Xu, Gui-yang
Wang, Chun-guang
Gong, Lun-kun
Wang, Jiang-ning
Source :
International Journal of Turbo & Jet-Engines; Mar2020, Vol. 37 Issue 1, p71-78, 8p
Publication Year :
2020

Abstract

The experiment system of pulse detonation engine is set up to investigate the acoustic signature of detonation acoustic. The research on detonation acoustic characteristic of pulse detonation engine in three kinds of working states, deflagration stage, detonation stage and external detonation stage, is carried out. Results from the test show that the maximal P<subscript>Impact</subscript>, P<subscript>Jet1</subscript>, τ<superscript>+</superscript> and τ<subscript>Interval</subscript> are obtained in external detonation stage. In deflagration stage, the concentrate of PDE acoustic signal energy is obvious. The energy of impulsive rise of impact noise and jet noise is an important part of PDE acoustic in deflagration stage. In detonation stage, a concentration of energy distribution is appeared in low frequency, and the energy of medium-high frequency is decreased. In external detonation stage, energy distribution is more concentrated in low frequency. The value of η<subscript>11</subscript>/η<subscript>5</subscript> can be used to detect the working state of pulse detonation engine. When η<subscript>11</subscript>/η<subscript>5</subscript> is less than 5, pulse detonation engine is in deflagration stage, however, when η<subscript>11</subscript>/η<subscript>5</subscript> is large than 5, pulse detonation engine is in detonation stage or external detonation stage. [ABSTRACT FROM AUTHOR]

Details

Language :
English
ISSN :
03340082
Volume :
37
Issue :
1
Database :
Complementary Index
Journal :
International Journal of Turbo & Jet-Engines
Publication Type :
Academic Journal
Accession number :
142543690
Full Text :
https://doi.org/10.1515/tjj-2018-0044