Recent developments in the research on pulse detonation engines

被引：295

作者：

Kailasanath, K ^{[1
]}

机构：

[1] USN, Res Lab, Ctr React Flow & Dynam Syst, Washington, DC 20375 USA

来源：

AIAA JOURNAL | 2003年 / 41卷 / 02期

关键词：

D O I：

10.2514/2.1933

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

Significant progress is noted in the research toward the development of pulse detonation engines for airbreathing and rocket applications. Thus, the development of advanced laser-based diagnostics has played a key role in the validation of numerical models. Several independent investigations are used to arrive at a converged value for the performance of an idealized PDE operating on an ethylene-oxygen mixture.

引用

页码：145 / 159

页数：15