首页|延伸段压强分布对双钟形喷管模态转换速率的影响机理

延伸段压强分布对双钟形喷管模态转换速率的影响机理

Influence mechanism of wall pressure distribution in extension section on the mode transition rate of dual-bell nozzles

扫码查看
为揭示延伸段压强分布对双钟形喷管模态转换过程的影响机理,采用仿真、试验和理论分析并举的方法,对不同延伸段压强分布的双钟形喷管的模态转换过程开展了研究.结果表明:当实际工作落压比大于最大理论分离落压比时,分离点在非负压强梯度的延伸段型面上稳定存在的落压比平衡条件被打破,故其模态转换过程随分离点的移动快速进行.同时,因落压比失衡机制的存在,快速模态转换构型在正/逆转换间存在迟滞现象.顺压梯度延伸段型面则能够满足分离点稳定存在所需的工况平衡条件,故模态转换过程缓慢,且在此过程中并无迟滞现象的出现.
In order to reveal the influence mechanism of pressure distribution in the extension section on the mode transition of the dual-bell nozzle,the mode transition process of the dual-bell nozzle with different wall pressure distribution in the extension sec-tion was studied by means of simulation,experiment and theoretical analysis.The analysis shows that,when the actual working pressure ratio is greater than the maximum theoretical separation pressure ratio,the pressure ratio equilibrium condition of the sepa-ration point on the non-negative pressure gradient contour is destroyed,so the mode transition occurs rapidly with the movement of the separation point.Meanwhile,due to the unbalance mechanism of the nozzle pressure ratio,the hysteresis between the positive/inverse mode transition is also found.However,the negative pressure gradient contour can meet the equilibrium condition required for the stable existence of the separation point,so the mode transition process is slow,and there is no hysteresis in this process.

dual-bell nozzleextended contourflow separationmode transitionhysteresis phenomenon

刘亚洲、李钰航、胡海峰、杨建文

展开 >

西安航天动力研究所,西安 710100

双钟形喷管 延伸段型面 流动分离 模态转换 迟滞现象

2024

固体火箭技术
中国航天科技集团公司第四研究院 中国宇航学会固体推进专业委员会

固体火箭技术

CSTPCD北大核心
影响因子:0.461
ISSN:1006-2793
年,卷(期):2024.47(1)
  • 26