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半挠性喷管挠性板弹性曲线计算方法 被引量:2

A Method of Calculating Elastic Curve of Semiflexible Plate Nozzle
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摘要 本文基于梁弯曲变形的小挠度线性理论,提出了半挠性喷管挠性板弹性曲线的计算方法。并对挠性板弹性曲线与气动力学给出的型面进行了对比研究,两者吻合得较好,研究表明,结构设计中撑杆合理布局,是影响匹配的关键问题,足应引起设计者的重视。 A method of calculating elastic curve for semiflexible plate wind tunnel nozzle has been presented, based on the linear theory of small deflection of beam deformation, in this paper. In light of the match results of curvature between flexible plate calculated and aerodynamic contour, the reasonable arrangment of jacks on the plate, which has an obvious effect on the curvature match, is of vital importance. So the structure designer of flexible nozzle should be cautious of it.
作者 刘铭甲
出处 《国防科技大学学报》 EI CAS CSCD 北大核心 1992年第2期109-114,共6页 Journal of National University of Defense Technology
关键词 计算方法 喷管 弹性曲线 挠性板 calculation method, flexible plate nozzle, elastic curve, curvature match
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同被引文献29

  • 1刘佳鑫,秦伟,周扬,胡知诿.半柔壁喷管喉块柔板接触力仿真分析[J].机械科学与技术,2020,0(1):22-27. 被引量:1
  • 2张晓伟,杨嘉陵.柔壁风洞设计中的Elastica反问题[J].航空学报,2005,26(6):696-700. 被引量:2
  • 3王一白,王长辉,刘宇,覃粒子.多单元圆转方塞式喷管的性能计算和分析[J].航空动力学报,2007,22(4):639-644. 被引量:2
  • 4Varner M O,Summers W E,Davis M W. A review of two- dimensional nozzle design techniques[AIAA Paper 82- 0609][R].1982.
  • 5LI Junwei,LIU Yu,LIAO Yunfei. Experimental and numerical study on two-dimensional plug nozzle[AIAA Paper 2010-6659][R].2010.
  • 6Erdmann S F. A new economic flexible nozzle for supersonic wind tunnels[J].Journal of Aircraft,1970,(01):58-60.
  • 7Ito T,Fujii K,Hayashi A K. Computations of axisymmetrie plug-nozzle flow-fields:flow structures and thrust performance[J].Journal of Propulsion and Power,2002,(02):254-259.
  • 8Mizukaki T,Watabe S. Flow visualization of starting process of a two-dimensional truncated plug nozzle using shock tube[AIAA Paper 2011-2315][R].2011.
  • 9Miyamoto H,Matsuo A,Kojima T. Effects of sidewall configurations on rectangular plug nozzle performance[AIAA Paper 2006-4373][R].2006.
  • 10Juhany K A,Husaini H E. Investigation of a aingle-jack flexible supersonic nozzle[AIAA Paper 2007-958][R].2007.

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