Journal
ACTA ASTRONAUTICA
Volume 189, Issue -, Pages 712-721Publisher
PERGAMON-ELSEVIER SCIENCE LTD
DOI: 10.1016/j.actaastro.2021.08.022
Keywords
Powdered engine; Solid-gas two-phase flow; Powder feeding; Mass flow rate; Gas-solid ratio
Categories
Funding
- National Natural Science Foundation of China [52006169]
- Xi'an Modern Chemistry Research Institute [SYJJ38]
Ask authors/readers for more resources
In this study on powdered engines, the optimal powder-feeding technique was investigated, with findings showing a high linear tendency between powder mass flow rate and the minimum throttle channel area. The solid-gas mass ratio for stable powder feeding was determined to be approximately in the range of 34.4-54.6 under different throttle channel areas.
It is a key and difficult problem to find the optimal powder-feeding technique in the study of powdered engines. In this paper, the feeding of powder in powder engines at different gas-solid ratios was experimentally investigated. Working characteristics of the classic piston-driven powder feeding system were obtained. A high linear tendency between powder mass flow rate and the minimum throttle channel area is observed from the experiment. The solid-gas mass ratio to maintain a stable powder feeding is approximately valued in range of 34.4-54.6 under different throttle channel areas. The least deviation in the relative powder mass flow rate for the tests is 15% to +8%. Due to the high uncertainty of the gas-solid flow structures at different gas-solid ratios, obvious low-frequency oscillations and high-frequency oscillations exist during the powder feeding process. The frequencies of low-frequency oscillations are mainly 1-3 Hz, while those of high-frequency oscillations are 20-30 Hz and 30-45 Hz in different tests.
Authors
I am an author on this paper
Click your name to claim this paper and add it to your profile.
Reviews
Recommended
No Data Available