| Citation: | ZHANG Xiao-qing, LE Jia-ling. Numerical study on the starting characteristics of the pulse combustion wind tunnel[J]. Journal of Aerospace Power, 2008, 23(9): 1568-1572.
|
| [1] |
乐嘉陵,刘伟雄,贺伟,等.脉冲燃烧风洞及其在火箭和超燃发动机研究中的应用[J].实验流体力学,2005,19(1):1-10.LE Jialing,LIU Weixiong,HE Wei,et al.Impulse combustion wind tunnel and its application in rocket and scramjet research[J].Journal of Experiments in Fluid Mechanics,2005,19(1):1-10.(in Chinese)
|
| [2] |
Yang G W,Hu Z M,Jiang Z.Starting nozzle flow simulation using K-G two-equation turbulence model[C]// Jiang Z ed.Proceedings of the 24th International Symposium on Shock Waves.Beijing:Springer,2004:1175-1180.
|
| [3] |
Jacobs P A.Numerical simulation of transient hypervelocity flow in an expansion tube[R].NASA-CR-189615,1992.
|
| [4] |
Jacobs P A.Simulation of transient flow in a shock tunnel and a high Mach number nozzle[R].NASA-CR-187606,1991.
|
| [5] |
Jacobs P A.Transient,hypervelocity flow in an axisymmetric nozzle[R].NASA-CR-187496,1991.
|
| [6] |
Fluent Inc.Fluent version user's guide[M].Lebanon,U S A:[s.n.] 2005.
|
| [7] |
李桦,范晓樯,丁猛.超声速扩压器中激波串结构的数值模拟[J].国防科技大学学报,2002,24(1):18-21.LI Hua,FAN Xiaoqiang,DING Meng.Numerical simulation of the shock train structure in the supersonic diffuser[J].Journal of National University of Deffense Technology,2002,24(1):18-21.(in Chinese)
|
DownLoad: