Hierarchical high-fidelity analysis methodology for buckling critical structures

被引:3
作者
Arbocz, J [1 ]
Starnes, JH
机构
[1] Delft Univ Technol, Fac Aerosp Engn, Delft, Netherlands
[2] NASA, Langley Res Ctr, Hampton, VA 23681 USA
关键词
buckling; thin shell structures; aerospace engineering; loads;
D O I
10.1061/(ASCE)0893-1321(2005)18:3(168)
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A hierarchical high-fidelity analysis methodology for predicting the critical buckling load of compression-loaded thin-walled isotropic shells is described. This hierarchical procedure includes three levels of fidelity for the analysis. Level I assumes that the buckling load can be predicted by the classical shell solution with simply supported boundary condition, and with a linear membrane prebuckling solution. Level 2 includes the effects of a nonlinear prebuckling solution and the effects of traditional clamped or simply supported boundary conditions. Level 3 includes the nonlinear interaction between nearly simultaneous buckling modes and the effects of boundary imperfections and general boundary conditions. Various deterministic and probabilistic approaches are used to account for the degrading effects of unavoidable shell-wall geometric imperfections. The results from the three solution levels are compared with experimental results, and the effects of the assumptions and approximations used for the three solution levels are discussed. This hierarchical analysis approach can be used in the design process to converge rapidly to an accurate prediction of the expected buckling load of a thin-shell design problem.
引用
收藏
页码:168 / 178
页数:11
相关论文
共 38 条
[1]  
ALMROTH BO, 1973, AFFDLTR718
[2]  
[Anonymous], THESIS
[3]  
[Anonymous], 1968, NASA
[4]   The effect of imperfect boundary conditions on the collapse behavior of anisotropic shells [J].
Arbocz, J .
INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES, 2000, 37 (46-47) :6891-6915
[5]   EFFECT OF GENERAL IMPERFECTIONS ON BUCKLING OF CYLINDRICAL SHELLS [J].
ARBOCZ, J ;
BABCOCK, CD .
JOURNAL OF APPLIED MECHANICS, 1969, 36 (01) :28-&
[6]   KOITER STABILITY THEORY IN A COMPUTER-AIDED ENGINEERING (CAE) ENVIRONMENT [J].
ARBOCZ, J ;
HOL, JMAM .
INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES, 1990, 26 (9-10) :945-973
[7]  
ARBOCZ J, 1982, BUCKLING SHELLS, P535, DOI DOI 10.1007/978-3-642-49334-8_19
[8]  
ARBOCZ J, 1998, P 39 AIAA ASME ASCE, P2941
[9]  
Arbocz J, 1992, LR695 DELFT U TECHN
[10]  
ARBOCZ J, 1980, CR3310 NASA