Buckling behavior of compression-loaded quasi-isotropic curved panels with a circular cutout

International Journal of Solids and Structures

Volumn 38, Issue 9, 2001, Pages 1495-1522

  Hilburger, Mark W ^a,c   Britt, Vicki O ^b   Nemeth, Michael P ^c  

^a NATIONAL RESEARCH COUNCIL   (United States)

^b GULFSTREAM AEROSPACE CORPORATION   (United States)

^c NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BUCKLING; COMPRESSION TESTING; COMPUTER SIMULATION; DEFORMATION; FINITE ELEMENT METHOD;

COMPRESSION LOADS; CURVED PANELS;

STRUCTURAL PANELS;

EID: 0035254336     PISSN: 00207683     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0020-7683(00)00114-1     Document Type: Article

References (17)

1. Janisse, T.C., Palazotto, A.N., 1983. Collapse analysis of composite panels with cutouts. In: Proceedings of the AIAA/ASME/ASCE/ AHS 24th Structures, Structural Dynamics, and Materials Conference, AIAA paper 83-0875.
2. Knight, N.F., Starnes, J.H. Jr., 1984. Postbuckling behavior of axially compressed graphite-epoxy cylindrical panels with circular holes. In: Proceedings of the 1984 ASME Joint Pressure Vessels and Piping/Applied Mechanics Conference.
3. Knight, N.F., Starnes, J.H. Jr., 1986. Postbuckling behavior of selected graphite-epoxy cylindrical panel loaded in compression. In: Proceedings of the AIAA/ASME/ASCE/AHS 27th Structures, Structural Dynamics, and Materials Conference, AIAA paper 86-0881-CP.
4. Lee, C.E., Palazotto, A.N., 1984. Nonlinear collapse analysis of composite cylindrical panels with small cutouts or notches. In: Proceedings of the AIAA/ASME/ASCE/AHS 25th Structures, Structural Dynamics, and Materials Conference. AIAA paper 84-0889.
5. Madenci, E., Barut, A., 1994. Pre- and postbuckling response of curved, thin, composite panels with cutouts under compression. International Journal for Numerical Methods in Engineering 37, 1499-1510.
6. Nemeth, M.P., 1988. Buckling behavior of compression-loaded symmetrically laminated angle-ply plates with holes. AIAA Journal 26 (3), 330-336.
7. Nemeth, M.P., 1990. Buckling and postbuckling behavior of square compression-loaded graphite-epoxy plates with circular cutouts. NASA TP-3007.
8. Nemeth, M.P., 1994. Nondimensional parameters and equations for buckling of anisotropic shallow shells. Journal of Applied Mechanics 61, 664-669.
9. Nemeth, M.P., 1996. Buckling and postbuckling behavior of laminated composite plates with a cutout. NASA TP-3587.
10. Nemeth, M.P., Starnes, J.H., Jr., 1998. The NASA monographs on shell stability design recommendations: a review and suggested improvements. NASA TP-1998-206290.
11. Park, K.C., 1975. An improved stiffly stable method for direct integration of nonlinear structural dynamics. Journal of Applied Mechanics 42, 464-470.
12. Rankin, C., Brogan, F., 1991. The computational structural mechanics testbed structural element processor ES5: STAGS shell element. NASA Contractor Report 4358.
13. Rankin, C.C., Brogan, F.A., Loden, W.A., Cabiness, H.D., 1999. STAGS Users Manual, version 3.0. Lockheed Martin Missiles and Space Co., Advanced Technology Center, Report LMSC P032594.
14. Riks, E., 1987. Progress in collapse analysis. Journal of Pressure Vessel Technology 109, 27-41.
15. Riks, E., Rankin, C.C., Brogan, F.A., 1996. On the solution of mode jumping phenomena in thin-walled shell structures. Computer Methods in Applied Mechanics and Engineering 136 (1-2), 59-92.
16. Snell, M.B., Morley, N.T., 1985. The compression buckling behaviour of highly curved panels of carbon fibre reinforced plastic. In: Proceedings of the Fifth International Conference on Composite Materials, ICCM vol. 5, 1327-1354.
17. Wilkins, D.J., 1975. Compression buckling tests of laminated graphite-epoxy curved panels. AIAA Journal 13 (4), 465-470.