Journal of Projectiles, Rockets, Missiles and Guidance >
Simulation and Analysis for Fluid Field of Frangible Cover Opening by Gas Jet
Received date: 2015-11-02
Online published: 2025-05-30
The fluid field of frangible cover opening by gas jet is complexly unsteady. In order to solve the problem caused by boundary changes of back cover after pressure arriving the opening condition, dynamic mesh was used to deal with its movement, and fragmental boundary conditions which can be modified one by one were used to simulate its break. Some different flow fields were analyzed with different boundary conditions. Comparison of the simulation results shows that the process of back cover opening which followed with break and movement is important to the wave's creation and transmission in launching canister.
Key words: frangible cover; gas jet; numerical simulation
JING Jianquan , FU Debin , WANG Xinxing , HAN Lei . Simulation and Analysis for Fluid Field of Frangible Cover Opening by Gas Jet[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2016 , 36(4) : 80 -82 . DOI: 10.15892/j.cnki.djzdxb.2016.04.021
| [1] | MUSSEY R A. Launch tube closure: US 4301708 [P]. 1981-11-24. |
| [2] | FORIS Victor G. Protective missile launch tube enclosure: US 6311604B1 P. 2001-11-06. |
| [3] | KAM T Y, WU J H, WANG W T. External failure pressure of a frangible laminated composite canister cover [J]. Composite Structures, 1999, 47(1): 563-569. |
| [4] | 傅德彬, 姜毅. 某导弹易碎盖的开启过程 [J]. 固体火箭技术, 2007, 30(4): 275-277. |
| [5] | POTSDAM M A, GURUSWAMY G P. A parallel multiblock mesh movement scheme for complex aeroelastic applications: AIAA 2001-0716 [R]. 2001. |
| [6] | 赵承庆, 姜毅. 气体射流动力学 [M]. 北京: 北京理工大学出版社, 1998: 30-35. |
| [7] | Fluent Inc. FLUENT6.2 Documentation [CD]. 2002. |
/
| 〈 |
|
〉 |