Review on Factors Affecting the Performance of pulse Detonation Engine

被引:2
|
作者
Tripathi, Saurabh [1 ]
Pandey, Krishna Murari [1 ]
机构
[1] NIT Silchar, Dept Mech Engn, Silchar 788010, Assam, India
来源
INTERNATIONAL CONFERENCE ON ELECTRICAL, ELECTRONICS, MATERIALS AND APPLIED SCIENCE | 2018年 / 1952卷
关键词
Pulse detonation engine; Obstacles; Blockage ratio; DDT; Flame acceleration; ROCKET ENGINE; FLAME ACCELERATION; WALL-TEMPERATURE; HEAT-TRANSFER; PROPAGATION; CHANNELS; NOZZLE; TUBE;
D O I
10.1063/1.5032052
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
Now a day's rocket engines (air-breathing type) are being used for aerospace purposes but the studies have shown that these are less efficient, so alternatives are being searched for these. Pulse Detonation Engine (PDE) is one such efficient engine which can replace the rocket engines. In this review paper, different researches have been cited. As can be observed from various researches, insertion of obstacles is better. Deflagration to Detonation(DDT) transition process is found to be most important factor. So a lot of researches are being done considering this DDT chamber. Also, the ignition chamber and ejector were found to improve the effectiveness of PDE. The PDE works with a range of Mach 0-4.Flame acceleration is also found to increase the DDT process. Use of valve and valveless engine has also been compared. Various other factors have been focused in this review paper which is found to boost PDE performance.
引用
收藏
页数:7
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