Real-Fluid Effects on Flame Structure and Stability of Transcritical Liquid-Oxygen/Methane Counterflow Multi-Branch Flames

Laminar counterflow multi-branch flames provide a canonical configuration for investigating interactions between oxidizer-rich and fuel-rich streams in liquid-oxygen/methane combustion systems. This study numerically investigates their flame structure and stability under transcritical conditions, with stability characterized by the extinction strain rate. Ideal-fluid (IF), partial real-fluid (PRF), and real-fluid (RF) models are compared to distinguish the effects of real-fluid thermodynamics and high-pressure transport corrections. The multi-branch flame comprises two premixed branches coupled with a central diffusion branch. Heat release from the premixed branches creates high-temperature plateaus that preheat the stagnation-region mixture and sustain the diffusion branch. Although the three models predict similar flame topologies, the IF model gives an extinction strain rate of 3.306 × 106 s−1, whereas both PRF and RF predict 3.256 × 106 s−1. Thus, the ideal-fluid treatment slightly overpredicts the extinction limit under the present reference condition, while high-pressure transport corrections influence the ignition location, peak temperature, and thermal diffusivity. Increasing pressure from 10 MPa to 40 MPa raises the extinction strain rate from 9.336 × 105 s−1 to 4.867 × 106 s−1 by strengthening heat release and reducing thermal diffusion from the high-temperature region. Oxidizer preheating markedly enhances flame stability, whereas fuel preheating has a weak effect. These findings establish the connection between real-fluid thermodynamics, branch interaction, and extinction stability, providing a physical basis for model selection, operating-condition optimization, and stability-margin assessment in transcritical liquid-oxygen/methane combustion systems.

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Publication Details

Journal
Aerospace
Published
2026-07-30
DOI
https://doi.org/10.3390/aerospace13080689
Primary Topic
Combustion and flame dynamics
Type
article
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article

Real-Fluid Effects on Flame Structure and Stability of Transcritical Liquid-Oxygen/Methane Counterflow Multi-Branch Flames

Shengfeng Luo, Ying Bai, Weidong Huang, Wenfeng Hu et al.
Aerospace
Combustion and flame dynamics
article

Real-Fluid Effects on Flame Structure and Stability of Transcritical Liquid-Oxygen/Methane Counterflow Multi-Branch Flames

Shengfeng Luo, Ying Bai, Weidong Huang, Wenfeng Hu, Pengyu Liu, Bo He
article en

Abstract

Laminar counterflow multi-branch flames provide a canonical configuration for investigating interactions between oxidizer-rich and fuel-rich streams in liquid-oxygen/methane combustion systems. This study numerically investigates their flame structure and stability under transcritical conditions, with stability characterized by the extinction strain rate. Ideal-fluid (IF), partial real-fluid (PRF), and real-fluid (RF) models are compared to distinguish the effects of real-fluid thermodynamics and high-pressure transport corrections. The multi-branch flame comprises two premixed branches coupled with a central diffusion branch. Heat release from the premixed branches creates high-temperature plateaus that preheat the stagnation-region mixture and sustain the diffusion branch. Although the three models predict similar flame topologies, the IF model gives an extinction strain rate of 3.306 × 106 s−1, whereas both PRF and RF predict 3.256 × 106 s−1. Thus, the ideal-fluid treatment slightly overpredicts the extinction limit under the present reference condition, while high-pressure transport corrections influence the ignition location, peak temperature, and thermal diffusivity. Increasing pressure from 10 MPa to 40 MPa raises the extinction strain rate from 9.336 × 105 s−1 to 4.867 × 106 s−1 by strengthening heat release and reducing thermal diffusion from the high-temperature region. Oxidizer preheating markedly enhances flame stability, whereas fuel preheating has a weak effect. These findings establish the connection between real-fluid thermodynamics, branch interaction, and extinction stability, providing a physical basis for model selection, operating-condition optimization, and stability-margin assessment in transcritical liquid-oxygen/methane combustion systems.

AerospaceVol. 13(8)
Space Engineering University (CN), Shenzhen Technology University (CN)
Openalex Percentile: Top 11%
Combustion and flame dynamics
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