Experimental investigation of a pulse detonation engine with a two-dimensional ejector

被引:19
作者
Allgood, D [1 ]
Gutmark, E
Rasheed, A
Dean, AJ
机构
[1] Univ Cincinnati, Dept Aerosp Engn & Engn Mech, Cincinnati, OH 45221 USA
[2] Gen Elect Global Res Ctr, Energy & Propuls Technol Lab, Niskayuna, NY 12309 USA
关键词
D O I
10.2514/1.8125
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A parametric study into the integration of a pulse detonation engine (PDE) with an ejector was performed. Highspeed shadowgraph visualizations of the flow inside the two-dimensional ejector provided a qualitative method of determining the performance of the integrated system. The performance was observed to be sensitive to the inlet geometry of the ejector as well as its axial position relative to the exhaust plane of the PDE. Significant levels of entrainment were obtained when the ejector's inlet was contoured, whereas flow separation reduced entrainment efficiency in the ejector with a straight thin inlet lip. Also, the high-speed shadowgraph visualizations showed that the entrainment produced by the PDE-ejector system could be modified by the presence of an exhaust nozzle on the PDE. Qualitative analysis of the high-speed images using the coherent structure velocimetry method was conducted to obtain pseudovelocity information.
引用
收藏
页码:390 / 398
页数:9
相关论文
共 11 条
[1]  
ALLGOOD D, 2002, 20020613 AIAA
[2]  
GROSCHEL E, 2003, 20034970 AIAA
[3]  
HOKE J, 2002, 20020615 AIAA
[4]  
JOHNSON WS, 1968, 68WAFE33 ASME
[5]  
Meyer T.R., 2002, 20023863 AIAA
[6]  
Paxson D, 2002, 38 AIAA ASME SAE ASE, P3915
[7]  
PORTER JL, 1979, R91100CR47A ATC VOUG
[8]  
RASHEED A, 2003, 20034971 AIAA
[9]  
Shehadeh R., 2003, 20034972 AIAA
[10]  
WILSON J, 2002, 20023632 AIAA