期刊文献+

组件组合方式对两相PDE总压损失和峰值压力影响 被引量:1

Effect of test-parts assembly modes on total pressure loss and peak pressure in two-phase pulse detonation engine
下载PDF
导出
摘要 为了提高脉冲爆震发动机(PDE)的综合性能,在冷态条件下研究了螺旋钝体组件和扰流片钝体组件的总压损失,同时研究了它们在不同工作频率下的爆震波压力,将两者结合起来进行比较,确定相应组件的损失是有效总压损失还是无效总压损失。研究表明:激波反射器能反射、会聚强激波,增加爆震波峰值压力,因此它的总压损失大部分为有效损失;对于两相混气,平面火焰发生器和中心锥的总压损失基本为无效损失;总体上讲,螺旋钝体组件优于扰流片钝体组件。 In order to improve the comprehensive performance of Pulse Detonation Engine(PDE) , the total pressure loss of spiral obstacle assembly and circular annular obstacle assembly was investigated under the environmental condition, while the pressure of detonation wave of two assemblies was also studied at various operation frequency. The results of the total pressure loss and detonation wave pressure were compared to determine whether their total pressure loss was effective or not. It is showed that the cone reflector assembly can reflect and focus strong shock waves and improve peak pressure of detonation wave, so its total pressure loss is mainly effective. The generator of quasi-plane waves (GQPW) and central cone total pres- sure loss is basically ineffective for two-phase mixture. As a whole,the performance of spiral obstacle assembly is better than that of circular annular obstacle assembly.
出处 《推进技术》 EI CAS CSCD 北大核心 2010年第1期99-104,110,共7页 Journal of Propulsion Technology
基金 国家自然科学基金资助项目(50776045)
关键词 脉冲爆震发动机 有效总压损失 无效总压损失 峰值压力 Pulse Detonation Engine Effective total pressure loss Ineffective total pressure loss Peak pressure
  • 相关文献

参考文献10

二级参考文献56

  • 1何小民,王家骅.气动阀式两相脉冲爆震发动机研究[J].航空学报,2004,25(6):529-533. 被引量:19
  • 2李建中,王家骅,范育新,张靖周,张义宁.脉冲爆震发动机最大净推力和最佳工作频率[J].推进技术,2004,25(6):543-548. 被引量:5
  • 3张义宁,王家骅,张靖周.多循环吸气式脉冲爆震发动机推力直接测量[J].推进技术,2006,27(5):459-462. 被引量:16
  • 4Lindstedt R P, Michels H J. Deflagration to detonation transitions and strong deflagrations in alkane and alkene air mixtures [J]. Combust Flame, 1989,76:169 - 181.
  • 5Schauer F, Stutrud J, Bradley R. Detonation initiation studies and performance results for pulsed detonation engine applications[ R]. AIAA 2001-1129.
  • 6Lee S Y, Conrad C, Watts J, et al. Deflagration to detonation transition study using simultaneous schlieren and OH PLIF images[ R]. AIAA 2000-3217.
  • 7Brophy C M. Detonation studies of JP-10 with oxygen and air for pulse detonation engine development[R] . AIAA 1999-3213.
  • 8Brophy C M, Netzer D W. Effect of ignition characteristics and geometry on the performance of a JP-10/O2 fueled pulse detonation engine[ R] . AIAA 99- 2635.
  • 9Brophy C M. Detonation studies of JP-10 with oxygen and air for pulse detonation engine development[ R] . AIAA 1999-3213.
  • 10Brophy C M, Sinibaldi J O, Netzer D W, et al. Operation of a JP-10/air pulse detonation engine[R]. AIAA 2000-3591.

共引文献35

同被引文献7

引证文献1

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部