Computational Study of Compact Ejector-Enhanced Resonant Pulse Combustors

Yungster, Shaye ; Paxson, Daniel E ; Perkins, Hugh D

关键词: COMBUSTION CHAMBERS;    FUEL COMBUSTION;    RAYLEIGH EQUATIONS;   

RP-ID  :  GRC-E-DAA-TN57291

学科分类：航空航天科学

美国|英语

来源: NASA Technical Reports Server

【 摘 要 】

Previous studies of Ejector-Enhanced Resonant Pulse Combustors considered configurations that were relatively long, making them difficult to incorporate in practical gas turbine engines. In the present study, more compact configurations are analyzed, focusing on the system pressure gain. The study shows that it is possible to reduce the length of both the pulse combustor and ejector components without compromising the device's performance. In fact, it is found that in several of the compact configurations analyzed, the system pressure gain actually increased, reaching pressure gain levels above 5%, significantly higher than those obtained in previous studies. The Rayleigh efficiency, which has been used in the past to characterize the performance of pulse combustors, is computed for several of the Ejector-Enhanced Resonant Pulse Combustor configurations. The Rayleigh efficiency is seen to correlate with both average combustor pressure and system pressure gain for a given configuration, however, it could not be used to compare different configurations.