The conveying stability of the powder propellant is significant for the feeding-system design and particle-combustion performance of powder engines. In this study, a nozzle structure was employed to increase the conveying stability in a pipeline. The gas–solid flow through the nozzle was visualized, and the pressure signals were analyzed using multiscale methods: the standard deviation, wavelet transform, and higher order statistics. The nozzle structure helped to reorganize the downstream gas–solid by accelerating the gas–solid two-phase flow. The results for the standard deviation indicated that the upstream was more stable and less affected by the downstream at higher fluidized pressures. Through wavelet analysis, the energy fraction of the frequency band was used to represent the gas–solid characteristics, and the particle collision and nonlinear drag of the gas–solid interaction represented by the low-frequency band were determined to be the main factors affecting the downstream stability. Additionally, a high fluidized pressure (>2 MPa) yielded a relatively stable downstream flow. The higher order statistics method provided a better result than the standard deviation because of its high resolution and strong noise suppression. The analysis results indicate that increasing the particle size enhances the downstream stability.
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October 2019
Research-Article
Multiscale Analysis of Powder-Propellant Conveying Stability Through a Nozzle
Haijun Sun,
Haijun Sun
Aircraft Engineering College,
Nanchang Hangkong University,
Nanchang 330063, China
e-mail: sunhaij1987@163.com
Nanchang Hangkong University,
Nanchang 330063, China
e-mail: sunhaij1987@163.com
1Corresponding author.
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Chunbo Hu,
Chunbo Hu
School of Astronautics,
Northwestern Polytechnical University,
Xi'an 710072, China
Northwestern Polytechnical University,
Xi'an 710072, China
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Yihua Xu
Yihua Xu
Aircraft Engineering College,
Nanchang Hangkong University,
Nanchang 330063, China
Nanchang Hangkong University,
Nanchang 330063, China
Search for other works by this author on:
Haijun Sun
Aircraft Engineering College,
Nanchang Hangkong University,
Nanchang 330063, China
e-mail: sunhaij1987@163.com
Nanchang Hangkong University,
Nanchang 330063, China
e-mail: sunhaij1987@163.com
Chunbo Hu
School of Astronautics,
Northwestern Polytechnical University,
Xi'an 710072, China
Northwestern Polytechnical University,
Xi'an 710072, China
Yihua Xu
Aircraft Engineering College,
Nanchang Hangkong University,
Nanchang 330063, China
Nanchang Hangkong University,
Nanchang 330063, China
1Corresponding author.
Contributed by the Fluids Engineering Division of ASME for publication in the JOURNAL OF FLUIDS ENGINEERING. Manuscript received July 7, 2018; final manuscript received March 30, 2019; published online May 8, 2019. Assoc. Editor: Philipp Epple.
J. Fluids Eng. Oct 2019, 141(10): 101302 (9 pages)
Published Online: May 8, 2019
Article history
Received:
July 7, 2018
Revised:
March 30, 2019
Citation
Sun, H., Hu, C., and Xu, Y. (May 8, 2019). "Multiscale Analysis of Powder-Propellant Conveying Stability Through a Nozzle." ASME. J. Fluids Eng. October 2019; 141(10): 101302. https://doi.org/10.1115/1.4043421
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