Zhang Zhimin, Li Jinqiu, Guo Yanyanget al. Computational Model of Progressive Failure in Composite Sandwich Structures[J]. Journal of Beijing University of Aeronautics and Astronautics, 1999, 25(5): 565-568. (in Chinese)
Citation: Mo Changyu, Yuan Hongjie. Design method for specification of force-limited vibration testing[J]. Journal of Beijing University of Aeronautics and Astronautics, 2011, 37(4): 439-445. (in Chinese)

Design method for specification of force-limited vibration testing

  • Received Date: 25 Jan 2010
  • Publish Date: 30 Apr 2011
  • The method based on the complex two degrees of freedom system(TDFS) mode to design the specification of force-limited vibration testing was proposed. In the method, dynamic sub-structure was adopted to calculate modal effective mass and modal residual mass of specimen structure and supporting structure.The complex TDFS model parameter of vibration system in different frequency bands was defined according to the distribution of mode effective mass in frequency domain.The force spectrum and acceleration spectrum of contact surface between specimen and supporting structure was defined with the excitation condition of supporting structure. Spectrum envelope is the force-limited vibration test profile. Simulation results demonstrate that the force-limited vibration test conditions defined by this method is much more reality on vibration environment than conventional acceleration test condition.

     

  • [1] Dharanipathi Vijayamohan Rao.Investigation of the semi-empirical method for force limited vibration testing .Quebec:Department of Mechanical and Industrial Engineering,Concordia University,2003 [2] NASA-HDBK-7005 Dynamic environmental criter[S] [3] Andre Cote,Ramin Sedaghati.Force limited vibration complex two degree of freedom system method[J].AIAA Journal,2004,42(6):1208-1218 [4] NASA-HDBK-7004B Force limited vibration testing[S] [5] Soucy Y,Dharanipathi V.Investigation of force limited vibration for reduction of overtesting[J].Journal of Spacecraft and Rockets,2006,43(4):866-876 [6] Scharton T.Force limited vibration testing monograph .NASA Reference Publ RP-1403,1997 [7] 邱吉宝,向树红,张正平.计算机构动力学[M].合肥:中国科学与技术大学出版社,2009 Qiu Jibao,Xiang Shuhong,Zhang Zhengping.Computational structures dynamics[M].Hefei: University of Science and Technology of China Press,2009(in chinese) [8] Davis Gregory L.An analysis of nonlinear stiffness and damping effects in force-limited random vibration testing .Houston:Rice University,1998
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