| Citation: | WANG Pei-yong, CHEN Ming, XING Fei, LI Qiong. CFD numerical simulation of Hyshot scramjet[J]. Journal of Aerospace Power, 2014, (5): 1020-1028.
|
| [1] |
科林·西格尔.超燃冲压发动机:过程和特性[M].张新国, 译.北京:航空工业出版社, 2009.
|
| [2] |
Curran E T, Heiser W H, Pratt D T.Fluid phenomena in scramjet combustion systems[J].Annual Review of Fluid Mechanics, 1996, 28:323-360.
|
| [3] |
Heiser W H, Pratt D T.Hypersonic airbreathing propulsion[M].Washington:AIAA Education Series, 1994.
|
| [4] |
Odam J.Scramjet experiments using radical farming[D].Brisbane, Australia:The University of Queensland, 2004.
|
| [5] |
Mudford N, Mulreany P.CFD calculation for intake-injection shock-induced combustion scramjet flight experiments[R].AIAA-2003-7034, 2003.
|
| [6] |
Fureby C, Chapuis M.CFD analysis of the Hyshot Ⅱ scramjet combustor[J].Proceedings of the Combustion Institute, 2011, 33(2):2399-2405.
|
| [7] |
Rubins P M, Rhodes R P Jr.Shock-induced combustion with oblique shocks, comparison of experiment and kinetic calculations[J].AIAA Journal, 1963, 1(12):2778-2784.
|
| [8] |
Mudford N R, Mulreany P J, McGuire J R, et al.CFD calculations for intake-injection shock-induced-combustion scramjet flight experiments[R].AIAA-2003-7034, 2003.
|
| [9] |
Odam J, Paull A.Radical farming in scramjets[J].Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 2007, 96:276-283.
|
| [10] |
Brindle A, Boyce R R, Neely A J.CFD analysis of an ethylene-fueled intake-injection shock-induced-combustion scramjet configuration[R].AIAA-2005-3239, 2005.
|
| [11] |
Wilcox D.Turbulence modeling for CFD[M].3rd ed.La Canada Flintridge, CA:DCW Industries, 2006.
|
| [12] |
Magnussen B, Hjertager B.On mathematical modeling of turbulent combustion with special emphasis on soot formation and combustion[J].Symposium (International) on Combustion, 1977, 16(1):719-729.
|
| [13] |
王培勇, 汪延鹏, 冯韬, 等.涡团耗散模型A值对模拟精度的影响[R].重庆:工程热物理学会燃烧学年会, 2013.
|
| [14] |
林志勇.高静温超声速预混气爆震与发展过程机理研究[D].长沙:国防科学技术大学, 2008. LIN Zhiyong.Research on detonation initiation and development mechanisms in elevated temperature supersonic premixed mixture[D].Changsha:National University of Defense Technology, 2008.(in Chinese)
|
| [15] |
Star J, Edwards J, Smart M, et al.Numerical simulation of scramjet combustion in a shock tunnel[R].AIAA-2005-0428, 2005.
|
| [16] |
Gardner A.Upstream porthole injection in a 2-D scramjet model[J].Shock Waves, 2002, 11(5):369-375.
|
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