Effect of equivalence ratio on the detonation noise characteristics of pulse detonation engine

Author:

Xu Gui-Yang1,Li Bao-Xing1,Li Hong-Yan1,Zhu Yan-Fang2,Guan Yi-Wen1,Zhang Jian-Xiong1

Affiliation:

1. Xi’an Modern Chemistry Research Institute , Xi’an 710065 , P. R. China

2. Xijing University , Xi’an 710065 , P. R. China

Abstract

Abstract The experimental system of pulse detonation engine (PDE) is set up to investigate the influence of equivalence ratios on detonation noise characteristics. The research results show that as the equivalence ratio increasing, the amplitudes of detonation noise in all angles and locations increase, and the tB also increases simultaneously, while the tA increases first and then decreases. The equivalence ratio also has a great influence on the intensity of the detonation noise signal in the frequency band of 10–100 Hz, which increases firstly and then decreases with the increase of the equivalence ratio, and the maximum value is obtained at equivalence ratio of 1.1. The results are of great significance to study the mechanism of detonation noise and promote the process of the engineering application.

Publisher

Walter de Gruyter GmbH

Subject

Aerospace Engineering

Reference17 articles.

1. McConnaughey, PK, Femminineo, MG, Koelfgen, SJ, Lepsch, RA, Ryan, RM, Taylor, SA. Launch propulsion systems roadmap (technology area 01). Washington, DC, The United States of America: National Aeronautics and Space Administration (NASA); 2012.

2. Hu, C-Q, Fan, W, Yan, C-J, Li, Q, Ye, B. Experimental study of the effect of equivalence ratio on performance of pulse detonation rocket engine. Mech Sci Technol Aero Eng 2011;26:1981–5.

3. Jiang, T, Weng, C-S. Effect of inlet temperature and equivalence ratio on working process of pulse detonation engine. J Aero Power 2007;31:29–37.

4. Glaser, A, Caldwell, N, Gutmark, E. Acoustic characterization of a pulse detonation engine. Report AIAA 2006-2453. In: 12th AIAA/CEAS aeroacoustics conference, Cambridge, Massachusetts; 2006. https://doi.org/10.2514/6.2006-2453.

5. Shaw, L, Harris, K, Schauer, F, Hoke, J. Acoustic measurements for a pulse detonation engine. Report AIAA 2005-2952. In: 11th AIAA/CEAS aeroacoustics conference, Monterey, California; 2005. https://doi.org/10.2514/6.2005-2952.

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