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脉冲爆震发动机喷管流动的数值模拟 被引量:12
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作者 李辉煌 杨基明 徐立功 《推进技术》 EI CAS CSCD 北大核心 2004年第6期553-556,共4页
为了研究喷管形状及充气状况对脉冲爆震发动机推进性能的影响,发展了基于有限速率基元化学反应模型的网格自适应有限体积程序,对影响脉冲爆震发动机推进性能主要过程进行了数值模拟,计算结果和相应的实验结果较为一致。锥形喷管的算例表... 为了研究喷管形状及充气状况对脉冲爆震发动机推进性能的影响,发展了基于有限速率基元化学反应模型的网格自适应有限体积程序,对影响脉冲爆震发动机推进性能主要过程进行了数值模拟,计算结果和相应的实验结果较为一致。锥形喷管的算例表明,不仅锥角对喷管性能有重要影响,而且同一锥角下喷管内的充气状况对喷管性能也有重要影响。在喷管内充空气情形下,爆轰波进入喷管后迅速衰减为激波,扩张管道的超声速膨胀使得喷管壁面压力显著下降,从而削弱了喷管提高脉冲爆震发动机推进性能的作用。在喷管内充燃气情形下,爆轰波进入喷管后可一直维持到喷管出口,显著提高了脉冲爆震发动机的推动性能。 展开更多
关键词 ^脉冲发动机^+ 喷管 流动 数值仿真
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脉冲爆震发动机多循环工作过程仿真及性能分析 被引量:6
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作者 邱华 严传俊 +1 位作者 熊姹 李强 《推进技术》 EI CAS CSCD 北大核心 2007年第3期296-301,共6页
针对脉冲爆震发动机零维性能模型的局限性,建立了火箭式脉冲爆震发动机(PDRE)多循环工作过程的一维非稳态仿真性能模型,仿真模型能够捕获PDRE的非定常的工作特征,可研究各种调节参数对PDRE性能的影响,通过模拟计算直管PDRE和带收敛扩张... 针对脉冲爆震发动机零维性能模型的局限性,建立了火箭式脉冲爆震发动机(PDRE)多循环工作过程的一维非稳态仿真性能模型,仿真模型能够捕获PDRE的非定常的工作特征,可研究各种调节参数对PDRE性能的影响,通过模拟计算直管PDRE和带收敛扩张喷管PDRE在多循环工作过程中的压力分布及其性能参数,可以看到,由于循环过程之间的耦合性,使得多循环脉冲爆震发动机(PDE)的内部流场与单循环PDE有很大的不同;同时,同样进气条件下,PDRE要比常规火箭发动机有优势,对其工作频率和隔离气体使用量是有要求的。 展开更多
关键词 推进系统 ^火箭式脉冲发动机^+ 一维性能模型
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Investigation of Detonative Combustion Characteristics 被引量:2
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作者 HAN Qi-xiang WANG Jia-hua WANG Bo 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2002年第2期72-76,共5页
The pressure and deflagration to detonation transition(DDT)characteristics of acetylene and oxygen flame were studied in a detonation tube.The pressure history and the flame velocity along the tube were measured with ... The pressure and deflagration to detonation transition(DDT)characteristics of acetylene and oxygen flame were studied in a detonation tube.The pressure history and the flame velocity along the tube were measured with high frequency pressure transducers and ion probes.By analyzing the data recorded in the experiment,the detonation wave pressure,post wave pressure and DDT distance were obtained,together with the effects of the initial pressure varying from 2×10^(4)Pa to 10^(5)Pa,equivalence ration from 0.3 to 1.0,and mixture concentration from 60%to 100%.It was found that the detonation pressure was decreased respectively with the decrease of initial pressure,equivalence ratio and mixture concentration,but the DDT distance was enlarged.The DDT distance was found particularly sensitive to mixture concentration. 展开更多
关键词 DETONATION COMBUSTION deflagration to detonation transition pulse detonation engine
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Numerical Investigation on Detonation Wave through U-bend 被引量:3
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作者 Shinobu Otsuka Masaya Suzuki Makoto Yamamoto 《Journal of Thermal Science》 SCIE EI CAS CSCD 2010年第6期540-544,共5页
Pulse detonation engine (PDE) is expected for a next-generation propulsion system. PDE is a promising engine that can generates power and thrust by using intermittent detonation. Promotion of deflagration to detonatio... Pulse detonation engine (PDE) is expected for a next-generation propulsion system. PDE is a promising engine that can generates power and thrust by using intermittent detonation. Promotion of deflagration to detonation transition (below DDT) is a key issue to realize this system. PDE has experimentally been investigated, and it was confirmed that detonation tubes with U-shaped bends are useful for fast DDT. However, the mechanism of DDT promotion due to U-bends has not been well clarified. In the present study, the influence of a U-bend on detona-tion wave propagation is researched with computational fluid dynamics (CFD). The numerical results show that detonation wave disappears once near the U-bend inlet and restarts after passing through it. In addition, it was found that the use of the U-bend with small channel width and curvature radius can induce fast DDT. 展开更多
关键词 DETONATION Deflagration to Detonation Transition (DDT) U-bend Computational Fluid Dynamics
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