Abstract
Tee-section columns have been tested under conditions that provide a close relationship between the results so obtained and the behavior of certain classes of stiffenedplate structures. It is shown that severe imperfection sensitivity arises when the overall column critical load is coincident, or nearly coincident, with the local torsional critical load of the stiffener. And, although the present results are clearly not directly applicable to stiffened-plate design, it is suggested that, it these systems are to be designed with even greater material efficiencies than at present, the interactive mechanics observed could acquire increasing design importance. Accordingly, suggestions are made as to the form of research needed to provide a rational basis for the design of such ‘optimized’ stiffened-plate structures.
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Abbreviations
- b :
-
spacing between stiffeners
- d :
-
depth of stiffeners
- D :
-
flexural rigidity of stiffener plate
- e :
-
eccentricity of axial load
- e o :
-
fabrication imperfection
- E :
-
modulus of elasticity
- F :
-
force in load cell
- F o :
-
initial force in load cell
- I :
-
second moment of area of T-section
- k :
-
constant used for local critical load
- ℓ:
-
wavelength of local critical mode—lateral stiffener spacing
- L :
-
length of model
- P :
-
axial load
- P b :
-
maximum or buckling load
- P crit :
-
minimum critical load
- P E :
-
overall or ‘Euler’ critical load
- P L :
-
local critical load
- P y :
-
uniform axial-compression yield load
- t :
-
thickness of stiffener and flange plates
- δ:
-
maximum overall deformation of model
- μ:
-
Poisson's ratio
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Ellinas, C.P., Kaoulla, P., Kattura, S. et al. Tests on interactive buckling of stiffened plates. Experimental Mechanics 17, 455–462 (1977). https://doi.org/10.1007/BF02324668
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DOI: https://doi.org/10.1007/BF02324668