Buckling and postbuckling behavior of stiffened composite panels loaded in compression

AIAA Journal

Volumn 35, Issue 1, 1997, Pages 202-204

  Lee, I C ^a,b   Kim, C G ^a,b   Hong, C S ^a,b  

^a Korea Advanced Institute of Science and Technology (KAIST)   (South Korea)

^b Department of Aerospace Engineering ^*  (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY CONDITIONS; BUCKLING; COMPOSITE STRUCTURES; CONSTRAINT THEORY; FAILURE (MECHANICAL); FAILURE ANALYSIS; FINITE ELEMENT METHOD; MATHEMATICAL MODELS; SHEAR STRESS; STIFFNESS; STRUCTURAL LOADS; STRUCTURAL PANELS;

COMPOSITE PANELS; COMPRESSION LOADING; STIFFENING;

AIRCRAFT PARTS AND EQUIPMENT;

EID: 0030736967     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.7436     Document Type: Article

References (7)

1. Dickson, J. N., Cole, R. T., and Wang, J. T. S.,"Design of Stiffened Composite Panels in the Post-Buckling Range," Fibrous Composites in Structural Design, edited by E. M. Lenoe, D. W. Oplinger, and J. J. Burke, Plenum, New York, 1980, pp. 313-327.
2. Sheinman, I., Frostig, Y, and Segal, A., "PBCOMP Program for Buckling and Postbuckling of Stiffened Laminated Curved Panels," Computers and Structures, Vol. 42, No. 1, 1992, pp. 87-95.
3. Starnes, J. H., Jr., Knight, N. F., Jr., and Rouse, M., "Postbuckhng Behavior of Selected Flat Stiffened Graphite-Epoxy Panels Loaded in Compression," AIAA Journal, Vol. 23, No. 8, 1985, pp. 1236-1246.
4. Lee, S., Elaldi, F, Villalobos, H., and Scott, R. F., "Experimental and Analytical Study of J-Stiffened Composite Panels Loaded in Axial Compression," Proceedings of 9th International Conference on Composite Materials (ICCM-IX) (Madrid, Spain), Woodhead Publishing, Cambridge, England, UK, 1993, pp. 519-526.
5. Jun, S. M., and Hong, C. S., "Buckling Behavior of Laminated Composite Cylindrical Panel with Initial Imperfections," Recent Developments in Buckling of Structures, PVP-Vol. 183, AD-Vol. 18, American Society of Mechanical Engineers, New York, 1989, pp. 9-15.
6. Kweon, J. H., and Hong, C. S., "An Improved Arc-Length Method for Postbuckling Analysis of Composite Cylindrical Panels," Computers and Structures, Vol. 53, No. 3, 1994, pp. 541-549.
7. Kweon, J. H., Hong, C. S., and Lee, I. C., "Postbuckling Compressive Strength of Graphite/Epoxy Laminated Cylindrical Panels Loaded in Compression," AIAA Journal, Vol. 33, No. 2, 1995, pp. 217-222.