Time-resolved exergy analysis and operating parameters optimization of pulse detonation combustor

• A novel time-resolved exergy analysis framework for pulse detonation combustor (PDC) is established. • Equivalence ratio is the most significant factor affecting exergy efficiency and equivalent specific exhaust exergy. • The non-filling phase contributes the vast majority of the cumulative exhaust exergy(>87%). • Response Surface Methodology identifies the optimal PDC operating parameters. The exergy of exhaust gases from pulse detonation combustor (PDC) is critical for pulse detonation engine performance. However, conventional cycle-averaged exergy analysis fails to capture the unsteady exhaust characteristics of PDC. To address this gap, this paper proposes a novel time-resolved exergy analysis method dynamically tracking transient flow unsteadiness, variable specific heat, and variable gas composition during exhaust process. Time-resolved and cumulative exhaust exergy were calculated using flow parameters from a zero-dimensional analytical PDC model. Exergy efficiency and equivalent specific exhaust exergy (ESEX) were employed as core performance metrics to investigate the effects of compressor pressure ratio (CPR), equivalence ratio ( ϕ ), and operating frequency ( f ). To validate the necessity of the proposed method, a systematic comparison with conventional cycle-averaged analysis was conducted. Furthermore, Response Surface Methodology (RSM) was employed for parameter influence analysis and optimization. The results indicated that: increased CPR reduced both metrics primarily due to elevated PDC inlet temperature; exergy efficiency peaked at ϕ = 0.8, while ESEX peaked at ϕ = 1.1; and increased operating frequency caused a linear decline in both metrics. In comparison, conventional cycle-averaged methods underestimated exergy efficiency and ESEX by approximately 10–20%. Notably, RSM identified ϕ as the most significant factor affecting performance metrics. Based on the RSM model, the optimal operating parameters were determined as CPR = 3, ϕ = 1.0, and f = 10 Hz, yielding a maximum exergy efficiency of 65.60% and ESEX of 2080.54 kJ/kg. These findings not only provide significant theoretical guidance for unsteady combustion gas exergy assessment, but also enable more accurate economic and environmental evaluations by eliminating the bias introduced by conventional methods.

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Publication Details

Journal
Thermal Science and Engineering Progress
Published
2026-02-22
DOI
https://doi.org/10.1016/j.tsep.2026.104605
Primary Topic
Combustion and Detonation Processes
Type
article
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article

Time-resolved exergy analysis and operating parameters optimization of pulse detonation combustor

Zhiyi Xiao, Kexin Liu, Longxi Zheng
Thermal Science and Engineering Progress
Combustion and Detonation Processes
article

Time-resolved exergy analysis and operating parameters optimization of pulse detonation combustor

Zhiyi Xiao, Kexin Liu, Longxi Zheng
article en

Abstract

• A novel time-resolved exergy analysis framework for pulse detonation combustor (PDC) is established. • Equivalence ratio is the most significant factor affecting exergy efficiency and equivalent specific exhaust exergy. • The non-filling phase contributes the vast majority of the cumulative exhaust exergy(>87%). • Response Surface Methodology identifies the optimal PDC operating parameters. The exergy of exhaust gases from pulse detonation combustor (PDC) is critical for pulse detonation engine performance. However, conventional cycle-averaged exergy analysis fails to capture the unsteady exhaust characteristics of PDC. To address this gap, this paper proposes a novel time-resolved exergy analysis method dynamically tracking transient flow unsteadiness, variable specific heat, and variable gas composition during exhaust process. Time-resolved and cumulative exhaust exergy were calculated using flow parameters from a zero-dimensional analytical PDC model. Exergy efficiency and equivalent specific exhaust exergy (ESEX) were employed as core performance metrics to investigate the effects of compressor pressure ratio (CPR), equivalence ratio ( ϕ ), and operating frequency ( f ). To validate the necessity of the proposed method, a systematic comparison with conventional cycle-averaged analysis was conducted. Furthermore, Response Surface Methodology (RSM) was employed for parameter influence analysis and optimization. The results indicated that: increased CPR reduced both metrics primarily due to elevated PDC inlet temperature; exergy efficiency peaked at ϕ = 0.8, while ESEX peaked at ϕ = 1.1; and increased operating frequency caused a linear decline in both metrics. In comparison, conventional cycle-averaged methods underestimated exergy efficiency and ESEX by approximately 10–20%. Notably, RSM identified ϕ as the most significant factor affecting performance metrics. Based on the RSM model, the optimal operating parameters were determined as CPR = 3, ϕ = 1.0, and f = 10 Hz, yielding a maximum exergy efficiency of 65.60% and ESEX of 2080.54 kJ/kg. These findings not only provide significant theoretical guidance for unsteady combustion gas exergy assessment, but also enable more accurate economic and environmental evaluations by eliminating the bias introduced by conventional methods.

Thermal Science and Engineering ProgressVol. 72
Northwestern Polytechnical University (CN), Aero Engine Corporation of China (China) (CN)
Affordable and clean energy
Openalex Percentile: Top 50%
Combustion and Detonation Processes
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