[an error occurred while processing this directive] [an error occurred while processing this directive]
[an error occurred while processing this directive]Journal of Projectiles, Rockets, Missiles and Guidance >
The CFD Simulation for Combustion Gas Port in Flow Control Device
Received date: 2015-07-02
Online published: 2025-05-30
In order to design the best mould surface of combustion gas port in flow control device, based on N-S equation, CFD simulation calculations were made by using Fluent program. By means of simulating fluid movement, the effects of different dilation angle on mixing flow-field were analyzed and theoretical scour of combustion gas port from the gas particle was obtained. The calculation shows that the design of combustion gas port with optimal dilation angle can effectively reduce gas outlet velocity. The result of calculation is elementarily consistent with experimental value.
Key words: flow control device; combustion gas port; simulation
ZHANG Quan , WANG Xiliang , LIU Leqing . The CFD Simulation for Combustion Gas Port in Flow Control Device[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2016 , 36(5) : 94 -96 . DOI: 10.15892/j.cnki.djzdxb.2016.05.024
| [1] | 关大林, 王宁飞. 改善硼粒子点火及燃烧性能研究的回顾与展望[J]. 火炸药学报, 1998 (2): 52- 54. |
| [2] | 王英红, 李进贤, 李葆萱,等. 含硼富燃料推进剂各组分对其低压燃速的影响[J]. 兵工学报, 2005, 26 (2): 274- 277. |
| [3] | VANKA S P, CRAIG R R, STULL F D. Mixing, Chemical reaction and flow field development in ducted rockets[J]. Jounal of Propulsion and Power, 1984, 2 (4): 331- 338. |
| [4] | CHERNG D L, YANG V, KUO K K. Numerical study of turbulent reacting flows in solid-propellant ducted rocket combustors[J]. Jounal of Propulsion and Power, 1989, 5 (6): 678- 685. |
| [5] | VIGOT C, BARDELLE L, NADAUD L. Improvement of boron combustion in a solid-fuel ram rocket: AIAA 86-1590[R]. 1986. |
| [6] | 陈懋章. 粘性流体动力学基础[M]. 北京: 高等教育出版社, 2002: 32- 38. |
/
| 〈 |
|
〉 |