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
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
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页码:145 / 159
页数:15
相关论文
共 125 条
[91]  
Musielak D.E., 1998, 983878 AIAA
[92]  
NALIM MR, 2001, 20013613 AIAA
[93]   INTERMITTENT DETONATION AS A THRUST-PRODUCING MECHANISM [J].
NICHOLLS, JA ;
WILKINSON, HR ;
MORRISON, RB .
JET PROPULSION, 1957, 27 (05) :534-541
[94]   EXPERIMENTS IN GAS-DYNAMICS OF EXPLOSIONS [J].
OPPENHEIM, AK ;
SOLOUKHI.RI .
ANNUAL REVIEW OF FLUID MECHANICS, 1973, 5 :31-58
[95]  
PAXSON DE, 2001, 20013465 AIAA
[96]   BOUNDARY-CONDITIONS FOR DIRECT SIMULATIONS OF COMPRESSIBLE VISCOUS FLOWS [J].
POINSOT, TJ ;
LELE, SK .
JOURNAL OF COMPUTATIONAL PHYSICS, 1992, 101 (01) :104-129
[97]  
POVINELLI L, 2001, 01S501 INT ASTR FED
[98]  
POVINELLI LA, 2001, INT S AIRBR ENG
[99]  
Roy G., 2001, INT C CONTR DET PROC
[100]  
ROY GD, 2001, INT S AIRBR ENG