Analyzing combustion performance of LOX/GCH4 pintle injector according to spray characteristics

This study aims to reveal the influence of Local Momentum Ratio (LMR) on the combustion efficiency of an LOX/GCH4 pintle injector from the perspective of spray characteristics. Hot fire tests were conducted to establish the relationship between combustion efficiency and LMR. The spray characteristics for different LMRs were simulated by the validated volume of fluid-to-discrete phase model method, taking into account the combustion chamber wall confinement. Subsequently, the difference in combustion efficiency was analyzed by comparing the spray simulation results of backpressure conditions similar to hot fire tests. The results indicate that combustion efficiency increased initially (LMR = 1.12 - 1.64) and then decreased (LMR>1.64). Quantitative analysis revealed a linear correlation ( R 2 = 0.95) between LMR and combustion efficiency within 1.12 < LMR < 1.64. As the LMR increased, the improvement in combustion efficiency was attributed to a wider spray distribution range and smaller droplet sizes. The area of the mantle recirculation zone that is detrimental to combustion decreased by approximately 38%, and the droplet size reduced from 37 μm to 16 μm. This effectively enhanced both the mixing of the propellant and the evaporation process. When the LMR exceeded the critical value (1.64 in this study), the impingement of liquid oxygen on the combustion chamber wall was confirmed via overheating discoloration marks on the inner surface of combustion chamber’s cylindrical section. The impingement of liquid oxygen on the combustion chamber wall increased the transport of liquid oxygen to the wall, directly reducing the mixing quality and combustion efficiency. The outcomes of this study provide the practical guidance for design and improvement in combustion efficiency of the pintle injector thrust chamber.

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Publication Details

Journal
Chinese Journal of Aeronautics
Published
2025-07-24
DOI
https://doi.org/10.1016/j.cja.2025.103716
Primary Topic
Advanced Combustion Engine Technologies
Type
article
Field-Weighted Citation Impact
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article

Analyzing combustion performance of LOX/GCH4 pintle injector according to spray characteristics

Peng Cheng, Jieru Peng, Qinglian Li, Xiao Bai et al.
Chinese Journal of Aeronautics
Advanced Combustion Engine Technologies
article

Analyzing combustion performance of LOX/GCH4 pintle injector according to spray characteristics

Peng Cheng, Jieru Peng, Qinglian Li, Xiao Bai, Ziguang Li
article en

Abstract

This study aims to reveal the influence of Local Momentum Ratio (LMR) on the combustion efficiency of an LOX/GCH4 pintle injector from the perspective of spray characteristics. Hot fire tests were conducted to establish the relationship between combustion efficiency and LMR. The spray characteristics for different LMRs were simulated by the validated volume of fluid-to-discrete phase model method, taking into account the combustion chamber wall confinement. Subsequently, the difference in combustion efficiency was analyzed by comparing the spray simulation results of backpressure conditions similar to hot fire tests. The results indicate that combustion efficiency increased initially (LMR = 1.12 - 1.64) and then decreased (LMR>1.64). Quantitative analysis revealed a linear correlation ( R 2 = 0.95) between LMR and combustion efficiency within 1.12 < LMR < 1.64. As the LMR increased, the improvement in combustion efficiency was attributed to a wider spray distribution range and smaller droplet sizes. The area of the mantle recirculation zone that is detrimental to combustion decreased by approximately 38%, and the droplet size reduced from 37 μm to 16 μm. This effectively enhanced both the mixing of the propellant and the evaporation process. When the LMR exceeded the critical value (1.64 in this study), the impingement of liquid oxygen on the combustion chamber wall was confirmed via overheating discoloration marks on the inner surface of combustion chamber’s cylindrical section. The impingement of liquid oxygen on the combustion chamber wall increased the transport of liquid oxygen to the wall, directly reducing the mixing quality and combustion efficiency. The outcomes of this study provide the practical guidance for design and improvement in combustion efficiency of the pintle injector thrust chamber.

Chinese Journal of AeronauticsVol. 39(1)
National University of Defense Technology (CN)
Affordable and clean energy
Openalex Percentile: Top 85%
Advanced Combustion Engine Technologies
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