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Study on Modal Test Method for Vibration Characteristics of the Cylindrical Structure Filled with Liquid

액체가 채워진 원통형 구조물의 진동 특성 규명을 위한 모달 시험 방법 연구

  • Kim, Gen-Sang (Department of Aerospace Engineering, Chungnam National University) ;
  • Kim, Mun-Guk (Department of Aerospace Engineering, Chungnam National University) ;
  • Kim, In-Gul (Department of Aerospace Engineering, Chungnam National University) ;
  • Park, Jae-Sang (Department of Aerospace Engineering, Chungnam National University) ;
  • Park, Soon-Hong (Launcher Structures and Materials Team, Korea Aerospace Research Institute)
  • Received : 2018.05.18
  • Accepted : 2018.07.31
  • Published : 2018.08.01

Abstract

In the case of launch vehicles using liquid fuel, natural frequency changes due to fuel consumption after launch, and a modal test is essential to investigate its effect. However, when relying on modal test to characterize the free vibration characteristics, the testing time is excessively increased and accuracy is reduced. Therefore, this paper suggests a modal test method with finite element analysis to overcome these drawbacks. A cylindrical structure filled with liquid are considered as a study model, and modal tests and finite element analyses are performed. The modal tests are conducted by an impulsive method using an impact hammer and accelerometers. Through the comparison of the modal test and the finite element analysis results, the validity of the proposed modal test method is verified. In addition, the free vibration characteristics and the tendency for the cylindrical structure according to the liquid filled ratio were investigated.

액체 추진 발사체는 발사 후 추진제 소모로 인하여 고유진동수가 변화하는데, 이에 대한 영향을 규명하기 위해서는 모달 시험이 필수적이다. 그러나 액체 추진 발사체는 액체 추진제에 의한 액체의 영향과 발사체 구조의 영향이 복합적으로 작용하여, 이를 규명하는 것은 매우 어렵다. 또한 모달 시험에만 의존하여 복합된 특성을 규명하는 경우, 시험에 소요되는 시간이 과도하게 증가하고 특정 모드와 특정 주파수의 판별 및 확인이 쉽지 않다. 본 논문에서는 이러한 단점을 보완하기 위해 유한요소 해석 결과를 이용한 모달 시험 방법을 제안하였다. 액체가 채워진 원통형 구조물을 연구 모델로 선정하여 모달 시험과 유한요소 해석을 수행하였다. 모달 시험은 충격 가진 방식으로 충격망치와 가속도계를 이용하여 수행하였다. 모달 시험과 유한요소 해석 결과 비교를 통해 제안한 유한요소 해석 결과를 이용한 모달 시험 방법의 타당성을 검증하였으며, 액체가 채워진 비율에 따른 원통형 구조물의 자유진동 특성과 그 경향성에 대해 고찰하였다.

Keywords

References

  1. Miller, R. P., and Gerus, T. F., Experimental Lateral Bending Dynamics of the Atlas-Centaur-Surveyor Launch Vehicle, NASA TM X-1837, 1969.
  2. Buherle, R. D., Templeton, J. D., Reaves, M. C., Horta, L. G., Gaspar, J. L., Bartolotta, P. A., Parks, R. A., and Lazor, D. R., "ARES I-X Launch Vehicle Modal Test Overview," Proceedings of the IMAC-XXVIII, Jacksonville, Florida, 2010.
  3. Youn, S. H., Jang, Y. S., Park, S. H., and Yi, Y. M., "Modal Test of EM and Modal Analysis of FM for KSR-III," Journal of Korea Society for Aeronautical and Space Sciences, Vol. 32, No. 2, 2004, pp.95-102. https://doi.org/10.5139/JKSAS.2004.32.2.095
  4. Watkins, J. D., and Clary, R. R., Vibrational Characteristics of Some Thin-walled Cylindrical and Conical Frustum Shells, NASA TN D-2729, 1965.
  5. Jalali, H., and Parvizi, F., "Experimental and Numerical Investigation of Modal Properties for Liquid-Containing Structures," Journal of Mechanical Science and Technology, Vol. 26, No. 5, 2012, pp.1449-1454. https://doi.org/10.1007/s12206-012-0336-4
  6. Lee, S., and Lee, J. W., "Investigation of Error Factors from an Impact Hammer Test for Developing a Statistic Based Technique for Model Updating," Transactions of the Korean Society of Mechanical Engineers A, Vol. 40, No. 2, 2016, pp.185-198. https://doi.org/10.3795/KSME-A.2016.40.2.185
  7. Leadbetter, S. A., Leonard, W., and Brock, E. J. Jr., Design and Fabrication Considerations for a 1/10-scale Replica Model of the Apollo/Saturn V, NASA TN D-4138, 1967.
  8. Johannes, W., "The Virtual Mass Method," Virtual Mass Seminar, MSC Corporation, 2002.
  9. Kim, G. S., Study on Free Vibration Characteristics of the Cylindrical Structure Filled with Liquid, MS Thesis, Department of Aerospace Engineering, Chungnam National University, 2017.
  10. Peter, A., "Experimental Modal Analysis," Sound and Vibration Magazine, 2001.