| Citation: | TAN Jian-guo, HUANG Guo-qing, PAN Yu, WANG Zhen-guo. Research on combustion efficiency of cavity-type ramjet[J]. Journal of Aerospace Power, 2011, 26(6): 1415-1419. |
| [1] |
Waltrup P J,White M E,Zarlingo F,et al.History of ramjet and scramjet propulsion development for U.S.navy missiles[J].Johns Hopkins APL Technical Digest,1997,18(2):234-243.
|
| [2] |
刘兴洲.飞航导弹动力装置[M].北京:国防工业出版社,1992.
|
| [3] |
李庆,潘余,谭建国,等.亚燃冲压发动机中凹腔与V槽火焰稳定器性能对比分析[J].航空动力学报,2010,24(1):35-40. LI Qing,PAN Yu,TAN Jianguo,et al.Comparison of characteristics of ramjet with cavity-based flameholder and V-gutter flameholder[J].Journal of Aerospace Power,2010,24(1):35-40.(in Chinese)
|
| [4] |
Samaniego J M,Yip B,Poinsot T,et al.Low-frequency combustion instability mechanisms in a side-dump combustor[J].Combustion and Flame,1993,94(4):363-380.
|
| [5] |
Roux A,Gicquel L Y M,Sommerer Y,et al.Large eddy simulation of mean and oscillating flow in a side-dump ramjet combustor[J].Combustion and Flame,2008,152(1-2):154-176.
|
| [6] |
Chen L,Lin R,Gu H,et al.Analyses of supersonic combustion by gas sampling .AIAA 2005-3317,2005.
|
| [7] |
Mitani T,Takahashi M,Tomioka S.Measurement of scramjet engine performance by gas sampling .AIAA 98-1590,1998.
|
| [8] |
McClinton C R,Anderson G Y.Evaluation of as bulk calorimeter and heat balance for determination of supersonic combustor efficiency .NASA TP 1739,1980.
|
| [9] |
刘国球.液 体火箭发动机原理[M].北京:宇航出版社,1993.
|
| [10] |
Kobayashi K,Tomioka S,Kato K,et al.Performance of a dual-mode combustor with multi-staged fuel injection .AIAA 2004-3482,2004.
|
| [11] |
Reggiori A,Riva G,Daminelli G B.A method for evaluating the combustion efficiency in direct connect supersonic combustion test facilities //Proceedings of 22nd International Symposium on Shock Waves.London,UK:Imperial College,1999:291-296.
|
| [12] |
Young G B W.Basic supersonic ramjet point-design performance .US Air Force,Research Memorandum,RM-1615,1955.
|