火 箭 发 动 机 燃 烧 室 中 燃 烧 噪 声 的 计 算 模 型

Translated title of the contribution: Calculation model of combustion noise in rocket motor chamber

Jiajin Zeng, Junwei Li*, Baoyin Ma, Chunjie Li, Ningfei Wang

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

Abstract

Combustion noise is generally divided into direct noise and indirect noise. The model of direct and indirect noises caused by unstable heat release in combustors with throat congestion is derived in time and frequency domain,respectively. The dissipation of entropy waves and attenuation of acoustic waves are considered. A combustor with unstable heat release is simplified as a straight tube heated by an electric heat source for theoretical calculation. Compared with the experimental results,the prediction error of the direct noise is smaller than 4%,and the trend of pressure disturbance is basically the same. Based on this model,the effects of pipe length and temperature disturbance on noise intensity are analyzed. The results show that the shorter pipe length causes larger intensity of direct and indirect noises,and the longer pipe length results in clearer separation between these two noises. The intensity of the direct noise and indirect noise increases linearly with the temperature disturbance,and the growth rate and intensity of the direct noise are twice that of the indirect noise without dissipation.

Translated title of the contributionCalculation model of combustion noise in rocket motor chamber
Original languageChinese (Traditional)
Article number128148
JournalHangkong Xuebao/Acta Aeronautica et Astronautica Sinica
Volume44
Issue number18
DOIs
Publication statusPublished - 25 Sept 2023

Fingerprint

Dive into the research topics of 'Calculation model of combustion noise in rocket motor chamber'. Together they form a unique fingerprint.

Cite this