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带单侧裂纹楔梁动力特性研究 被引量:2

DYNAMIC BEHAVIOUR INVESTIGATION OF TAPER BEAM WITH SIDEWISE CRACK
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摘要 由于裂纹存在引起构件局部柔度的变化,本文用线弹性断裂力学理论导出裂纹所释放的应变能,由Castigliano 定理得出局部柔度矩阵诸元素,据此来修正楔形梁的刚度矩阵,借助梁有限单元法,求解带裂纹楔形梁的动力特性,并对裂纹相对深度、裂纹位置、梁的长宽比、宽厚比。 Emergence of crack causes local flexibility variation of the component.A linear elasticity theory of fracture mechanics is applied to deriving the strain energy released by the crack.According to Castigliano theorem,elements of local flexibility matrix are obtained,which can correct the stiffness matrix of the taper beam.The dynamic behaviour of the taper beam has been found out by means of finite element method.The effects of relative depth of crack,crack location,ratios of length to width and width to taper thickness on natural frequency have been numerically investigated and the relevant experiments have been conducted to testify the calculation results.
作者 邢德顺
机构地区 燃气涡轮研究院
出处 《航空动力学报》 EI CAS CSCD 北大核心 1999年第4期371-374,共4页 Journal of Aerospace Power
关键词 振动 裂纹 柔软度 动力特性 叶片 航空 Beams Vibration Crack Flexibility
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参考文献2

  • 1周松江.变截面裂纹构件振动试验研究报告[M].航空航天部燃气涡轮研究所,1988..
  • 2周松江,变截面裂纹构件振动试验研究报告,1988年

同被引文献25

  • 1杨智春,于哲峰.结构健康监测中的损伤检测技术研究进展[J].力学进展,2004,34(2):215-223. 被引量:63
  • 2Wei S T,Pierre C. Localization Phenomena in Mistuned Assemblies with Cyclic Symmetry, Part 1:Free Vibrations [J]. ASME, Journal of Vibration, Acoustics, Stress, and Reliability in Design, 1988,110 : 429-438.
  • 3Bladeh R, Castanier M P, Pierre C. Reduced Order Modeling and Vibration Analysis of Mistuned Bladed Disk Assemblies with Shrouds[J]. Journal of Engineering for Gas Turbines and Power, 1999, 121 (3): 515- 522.
  • 4Bernstein H L, Alien J M. Analysis of Cracked Gas Turbine Blades[J]. Journal of Engineering for Gas Turbines and Power, 1992,114(2) : 293-301.
  • 5Walls D P,Delaneuville R E,Cunningham S E. Damage Tolerance Based Life Prediction in Gas Turbine Engine Blades under Vibratory High Cycle Fatigue[J]. Journal of Engineering for Gas Turbines and Power, 1997,119 (1) :143-146.
  • 6Wicks B J, Antoniou R A. An Investigation of Fatigue Failures of Turbine Blades in a Gas Turbine Engine by Mechanical Analysis[J]. Engineering Failure Analysis, 2002,9(2) :201-211.
  • 7Wauer J. Dynamics of Cracked Rotating Blades[J]. Applied Mechanics Reviews, 1991,44(11):273-278.
  • 8Dimarogonas A D. Vibration of Cracked Structures: A State of Art Review[J]. Engineering Fracture Mechanics,1996,55(5) : 831-857.
  • 9Fang X,Tang J. Crack Induced Vibration Localization in Simplified Bladed-disk Structures[J]. Journal of Sound and Vibration,2006,291(2):395-418.
  • 10Hou J F. Cracking Induced Mistuning in Blade Disks [J]. AIAA Journal, 2006,44 (11) : 2542-2546.

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