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Numerical Evaluation of Varying Combustion Chamber Length on the Performance of Pulse Detonation Engine Using DES Model (May, 10.1007/s42405-024-00746-0, 2024)
被引:0
|作者:
Pallela, Arvind
[1
]
Kumar, Shivam
[2
]
Thakur, Amit Kumar
[1
]
Gupta, Lovi Raj
[1
]
Singh, Rajesh
[3
]
机构:
[1] Lovely Profess Univ, Phagwara 144001, Punjab, India
[2] Punjab Engn Coll, Dept Aerosp Engn, Chandigarh, India
[3] Uttaranchal Univ, Uttaranchal Inst Technol, Dehra Dun 248007, Uttarakhand, India
关键词:
Combustion;
Detached eddy simulation;
Numerical simulation;
Pulse detonation;
D O I:
10.1007/s42405-024-00764-y
中图分类号:
V [航空、航天];
学科分类号:
08 ;
0825 ;
摘要:
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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页码:1603 / 1603
页数:1
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