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논문 기본 정보
- 자료유형
- 학술저널
- 저자정보
- 저널정보
- 한국항공우주학회 International Journal of Aeronautical and Space Sciences International Journal of Aeronautical and Space Sciences Volume.18 Number.3
- 발행연도
- 2017.9
- 수록면
- 450 - 466 (17page)
- DOI
- 10.5139/IJASS.2017.18.3.450
이용수
초록· 키워드
오류제보하기
This paper defines the modified effective membrane stiffness, bending stiffness considering the directionally dependent mechanical properties and mode shape function of a composite lattice rectangular plate, which is assumed to be a Kirchhoff- Love plate. It subsequently presents an approximate method of conducting a buckling analysis of the composite lattice rectangular plate with various boundary conditions under uniform compression using the Ritz method. This method considers the coupled buckling mode as well as the global and local buckling modes. The validity of the present method is verified by comparing the results of the finite element analysis. In addition, this paper performs a parametric analysis to investigate the effects of the design parameters on the critical load and buckling mode shape of the composite lattice rectangular plate based on the present method. The results allow a database to be obtained on the buckling characteristics of composite lattice rectangular plates. Consequently, it is concluded that the present method which facilitates the calculation of the critical load and buckling mode shape according to the design parameters as well as the parametric analysis are very useful not only because of their structural design but also because of the buckling analysis of composite lattice structures.
목차
Abstract
1. Introduction
2. Problem statement and analysis
3. Verification of the present method via finite element analysis
4. Parametric analysis for the buckling characteristics of the composite lattice rectangular plate
5. Conclusion
References
참고문헌 (22)
참고문헌 신청
Vasiliev, V. V., Barynin, V. A. and Razin, A. F., “Anisogrid composite lattice structures ? Development and aerospace applications”, Composite Structures, Vol. 94, 2012, pp. 1117- 1127.
Aoki, T., Yokozeki, T. and Yoshino, S., “Mechanical behavior of composite lattice cylinders”, 55th AIAA/ASMe/ ASCE/AHS/SC Structures, Structural Dynamics, and Materials Conference, 2014, pp. 1-8.
Zhang Y., Xue Z., Chen L. and Fang D., “Deformation and failure mechanisms of lattice cylindrical shells under axial loading”, Journal of Mechanical Sciences, Vol. 51, No. 3, 1993, pp. 213-221.
Frulloni E., Kenny J. M., Conti P. and Torre L., “Experimental study and finite element analysis of the elastic instability of composite lattice structures for aeronautic applications”, Composite Structures, Vol. 78, No. 4, 2007, pp. 519-528.
Morozov E. V., Lopatin A. V. and Nesterov V. A., “Finite element modelling and buckling analysis of anisogrid composite lattice cylindrical shells”, Composite Structures, Vol. 93, No. 2, 2011, pp. 308-323.
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