期刊文献+

推力矢量发动机燃气舵绕流场数值分析 被引量:2

Numerical Analysis of Circumferential Flow Field of Thrust Vector Motor et Vane
下载PDF
导出
摘要 该文以推力矢量发动机的燃气舵绕流场为研究对象,采用数值分析技术,确定了数值模拟的流动方程以及适合的RNG k-ε湍流模型,对包含舵基、舵片和发动机壳体在内的区域进行了计算。结果揭示了舵基、舵片附近的流动状况和特点,所得结论可以为舵基、舵片的结构设计、安装方式以及控制机构设计提供有益借鉴。通过与试验现象对比,反映出数值计算的结果在一定程度上可以满足工程分析的需要。 The circumferential flow field of the thrust vector motor et vane is studied by the numerical analysis. The simulation flow equations and RNG k - ε turbulence model were set up. The calculated results from the vane base, vane patch , and motor shell present the flow status and properties of the flow around the vane base and vane patch. The results are helpful to the structure design, installation and control design of et vane. The comparision with the experimental results shows that the mathematical simulation satisfies the need of the engineering analysis.
出处 《南京理工大学学报》 EI CAS CSCD 北大核心 2005年第5期532-535,共4页 Journal of Nanjing University of Science and Technology
关键词 推力矢量 燃气舵 数值模拟 绕流场 thrust vector et vane numerical simulation circumferential flow field
  • 相关文献

参考文献8

二级参考文献12

  • 1张福祥.火箭燃气射流动力学[M].北京:国防工业出版社,1988.55-57.
  • 2王存山.航空发动机的预研与推力矢量技术[J].国际航空,2000,.
  • 3陈懋章.粘性流体动力学基础[M].北京:高等教育出版社,1993..
  • 4[1]Cuffel R F, Back H L, Massier P F. Transonic flowfield in a supersonic nozzles with small throat radius of curvature. AIAA Journal, 1969,7(7):1364~1368
  • 5[2]Marcum D L, Hoffman J D. Numerical boundary condition procedures for Euler solvers. AIAA Journal, 1987,25(8):1054~1062
  • 6[3]Driakis D, Tsangaris S. Real gas effects for compressible nozzle flows. Journal of Fluid Engineering, 1993,115:115~120
  • 7[4]Riedebauch S, Weiland C. Inviscid Laval-nozzle flowfield calculation. Journal of Spacecraft,1988,25(1)
  • 8[5]Yang J Y. High-resolution nonscillatory schemes for unsteady compressible flows. AIAA J, 1992,30(6):1570~1575
  • 9Carson G T Jr, Caponc F J. Static internal performance of an axisyrmnctric nozzle with multiaxis thrust-vectoring capability[ R] . NASA Technical Memorandum 4237,1991.
  • 10Barth T J, Jespersen D. The design and application of upwind schemes on unstructured meshes[ R]. AIAA 89-0366.

共引文献51

同被引文献21

  • 1侯清海.空空导弹燃气舵气动设计技术综述[J].航空兵器,2000,7(6):37-40. 被引量:11
  • 2黄知涛,王茉瑚.微型涡喷发动机辐板热变形故障分析[J].机械科学与技术,2000,19(z1):89-90. 被引量:1
  • 3刘志珩.固体火箭燃气舵气动设计研究[J].导弹与航天运载技术,1995(4):9-17. 被引量:26
  • 4潘育松,徐永东,陈照峰,成来飞,张立同,熊党生.碳/碳化硅燃气舵的烧蚀及抗热震性[J].中国有色金属学报,2006,16(6):976-981. 被引量:6
  • 5益小苏,杜善义,张立同.中国材料工程大典第10卷复合材料工程[M].北京:化学工业出版社,2006:553-675.
  • 6A A 希什科夫等著,关正西,赵克喜泽.固体火箭发动机工作过程[M].北京:北京宇航出版社,2006.
  • 7Cho H H,et al. Analysis of particle laden flows around a jet vane in a solid rocket motor[ A ]. 37th American Institute of Aeronautics and Astronautics/American Society of Mechanical Engineers/Society of Automotive Engineers/American Society for Engineering Education Joint Planning Council Conference and Exhibit[C], July 2001 ,Salt Palace -Salt Lake City, Utah.
  • 8Yu M S, et al. A Study on a surface ablation of the jet vane system in a rocket nozzle[ A]. 37th American Institute of Aeronautics and Astronautics Thermophysics Conference [ C ], 28 June-I July 2004, Portland, Oregon, AIAA 2004-2276.
  • 9Ports R L . Application of integral methods to ablation charring erosion, a review[J]. Journal of Spacecraft and Rockets, 1995,32(2).
  • 10EI-Hija A H, et al. Cost Analysis for the Manufacture of C/C-SiC Structural Parts[ M]. Weinheim: WileyVCH, 2001.

引证文献2

二级引证文献2

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