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分流式气动阀流阻及雾化特性研究

The Research on Flow Drag and Atomization Characteristics of Shunt Aerodynamic Valve
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摘要 为研究一种新型气动阀—分流式气动阀的工作性能,文中在对该新型气动阀的工作机理进行分析的基础上,利用二维数值模拟方法研究了该气动阀的流阻和雾化特性,并将计算结果与钝体式气动阀进行对比。研究结果表明:相同条件下,分流式气动阀较钝体式气动阀的流阻特性要好,前者的效率大约是后者的1.84倍,此外,采用分流式气动阀的燃油雾化效果要明显优于钝体式气动阀。故可以得出以下结论:分流式气动阀的工作性能优于钝体式气动阀。 To research the performance of a new type of aerodynamic valve,a shunt aerodynamic valve,the flow drag and atomization characteristics of the new type aerodynamic valve were studied by numerical simulation based on the analysis of its working mechanism,and the calculated results were compared with the blunt block aerodynamic valve.The results show that the flow drag characteristic of the shunt aerodynamic valve is better than that of the blunt block aerodynamic valve,and the former efficiency is about 1.84 times as high as the latter one.Besides,the effect of fuel atomization using shunt aerodynamic valve is better than that of using blunt block aerodynamic valve.So,the performance of the shunt aerodynamic valve is better than that of the blunt block aerodynamic valve.
出处 《弹箭与制导学报》 CSCD 北大核心 2013年第3期91-94,118,共5页 Journal of Projectiles,Rockets,Missiles and Guidance
基金 国防十二五重点预研基金资助
关键词 脉冲爆震发动机(PDE) 分流 气动阀 数值方法 流阻及雾化特性 pulse detonation engine(PDE) shunt aerodynamic valve numerical method flow drag and atomization characteristics
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参考文献12

  • 1Helman D. Detonation pulse engine, AIAA 8621683[R]. 1986.
  • 2Hinkey J. Rotary 2valved muhiple 2cycle pulse detonation engine experimental demonstration, AIAA 9722746 [R]. 1997.
  • 3韩启祥.[D].南京:南京航空航天大学,2004,61~75.
  • 4Srnimov N N. Control of detonation onset in combustion ga- ses [ C ]//High Speed Deflagration and Detonation: Funda- mentals and Control, Moscow: ELEX-KM Publishers, 2001 : 3 - 30.
  • 5Ashasov O V, Penyazkov O G. Some gas dynamic methods for control of detonation initiation and propagation, AIAA 200123614[ R]. 2001.
  • 6Levin V A. A new approach to organizing operation cycles in pulse detonation engines [ C]//High Speed Deflagration and Detonation: Fundamentals and Control, Moscow: EL- EX-KM Publishers, 2001:223 - 238.
  • 7Brophy C M, Netzer D W, Forester D. Detonation studies of JP210 with oxygen and air for pulse detonation engine de- velopment, AIAA 9824003[ R]. 1995.
  • 8范育新,王家骅,李建中,张靖周.脉冲爆震发动机净推力系数研究[J].南京航空航天大学学报,2004,36(3):273-277. 被引量:9
  • 9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
  • 10何小民,王家骅.气动阀对脉冲爆震发动机爆震性能的影响研究[J].南京航空航天大学学报,2005,37(1):97-100. 被引量:5

二级参考文献42

  • 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何小民,王家骅.气动阀对脉冲爆震发动机爆震性能的影响研究[J].南京航空航天大学学报,2005,37(1):97-100. 被引量:5
  • 3韩启祥.[D].南京:南京航空航天大学,2004,61~75.
  • 4Helman D. Detonation pulse engine[R]. AIAA 86-1683,1986.
  • 5Hinkey J. Rotary-Valved ,Multiple-Cycle,Pulse detonation engine experimental demonstration[R]. A-IAA 97-2746,1997.
  • 6Kentifield J A C. The noise producing characteristics of highly loaded valveless pulse combustor [R].ASME 86-WA/NCA-34 DEC, 1986, 103- 109.
  • 7Bertin J H. Aerodynamic valved [P]. U.S. Patent No. 2,670,011,54,1984.
  • 8Wislicenus G F. Flow control means for pulsejet combustion units[P]. US Patent No. 2,618,925,52,1982.
  • 9Srnirnov N N. Control of detonation onset in combustion gases [A]. High-Speed Deflagration and Detonation: Fundamentals and Control [C].Moscow, 2001.3-30.
  • 10Ashasov O V, Penyazkov O G. Some gasdynamic methods for control of detonation initiation and propagation[R]. AIAA 2001-3614,2001.

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