| Citation: | ZHOU Jian-xing, PIAO Ying, QI Xing-ming, ZHU Jian-hong, CHEN Mei-ning. 3-D numerical investigation on supersonic combustion of hydrogen in two different type of scramjet combustors[J]. Journal of Aerospace Power, 2008, 23(3): 470-475.
|
| [1] |
刘陵,刘敬华,张榛,等.超声速燃烧和超声速燃烧发动机[M].西安:西北工业大学出版社,1993.
|
| [2] |
Vinagradov V,Grachev V,Petrov M.Experimental investigation of 2-D dual mode scramjet with hydrogen fuel at Mach 4～6[R].AIAA 90-5269.
|
| [3] |
Owens M G,Tehranian S,Segal C.Flame-holding configuration for combustion in Mach 1.8 airflow[J].Journal of Propulsion and Power,1998,14(4):456-461.
|
| [4] |
Voland R T,Auslender A H,Smart M K,et al.CIAM/ NASA Mach 6.5 scramjet flight and ground test[R].AIAA 99-4848.
|
| [5] |
Roudakov A S,Semenov V L,Hicks J W.Recent flight test results of the joint CIAM-NASA Mach 6.5 scramjet flight program[R].NASA/TP 1998-206548.
|
| [6] |
刘敬华,凌文辉,马祥辉,等.超声速燃烧室流场的数值模拟研究[J].推进技术,1999,20(2):28-32.LIU Jinghua,LING Wenhui,MA Xianghui,et al.Numerical simulation study of scramjet flow fieldFJ].Journal of Propulsion Technology,1999,20(2):28-32.
|
| [7] |
崔玉峰,徐刚,黄伟光.后台阶喷氢加喷空气超声速燃烧数值模拟[J].航空学报,2004,25(2):113-116.CUI Yufeng,XU Gang,HUANG Weiguang.Numerical simulation on supersonic combustion over a reward facing step with transverse hydrogen and air injection[J].Acta Aeronautica et Astronautica Sinica,2004,25 (2):113-116.
|
| [8] |
Evan J S,Schexnayder C J.Influence of chemical kinetics and unmixedness on burning in supersonic hydrogen flames[J].AIAA Journal,1980,18(2):188-193.
|
| [9] |
王春,司徒明,马继华,等.高温富油燃气超声速燃烧数值模拟[J].推进技术,2000,21(2):60-63.WANG Chun,SITU Ming,MA Jihua,et al.Numerical simulation on supersonic combustion of fuel-rich hot gas[J].Journal of Propulsion Technology,2000,21(2):60-63.
|
DownLoad: