Numerical Evaluation of Varying Combustion Chamber Length on the Performance of Pulse Detonation Engine Using DES Model
A two-dimensional detached eddy simulation was performed to investigate the behavior of a detonation wavelet in a pulse detonation engine. A chemical kinetic reactive flow of acetylene and oxygen was introduced into the simulation to analyze the reactive flow dynamics of two different models. A comp...
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Veröffentlicht in: | International journal of aeronautical and space sciences 2024, 25(4), , pp.1343-1360 |
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Hauptverfasser: | , , , , |
Format: | Artikel |
Sprache: | eng |
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Zusammenfassung: | A two-dimensional detached eddy simulation was performed to investigate the behavior of a detonation wavelet in a pulse detonation engine. A chemical kinetic reactive flow of acetylene and oxygen was introduced into the simulation to analyze the reactive flow dynamics of two different models. A comparative study was conducted on the detonation flow dynamics by varying the combustion chamber length. A comprehensive time-transient simulation with computation-intensive iterations was conducted to study the slightest change in the detonation wave characteristics. The results of the simulations suggest that a shorter combustion chamber in Model A provided a sustainable detonation. In comparison, Model B, with a longer combustion chamber, provided a dual detonation wave, which resulted in increased flow frequency of the detonation wave. |
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ISSN: | 2093-274X 2093-2480 |
DOI: | 10.1007/s42405-024-00746-0 |