ABSTRACT Results are presented of 8 tests on long stiffened panels under axial compression until collapse. The specimens are three bay panels with associated plate made of very high tensile steel S690. Four different configurations are considered for the stiffeners, which are made of mild or high tensile steel for bar stiffeners and mild steel for 'L' and 'U' stiffeners. The influence of the stiffener's geometry on the ultimate strength of the stiffened panels under compression is analyzed. This series of experiments belong to an extended series of tests that include short and intermediate panels which allows analyzing the effect of space framing on the strength of stiffened panels
Buckling and postbuckling of plates and stiffened panels are considered. Computational models for di...
ABSTRACTThis paper concentrated on the ultimate uniaxial compressive strength of stiffened panel wit...
Stiffened composite panels are primary structural components in ship, aircraft and aerospace vehicle...
The results of 8 tests on panels under axial compression until collapse are presented. The panels ar...
of the Institute of Aerophysics for providing the opportunity of carrying out this investigation. Th...
An analysis for determining the effects of eccentricities and lateral pressure on the design of stif...
The aim of this research was to find design data for the stiffened plywood panels supplied by the Fl...
As the steel is tested for all types of tests viz, compressive, tensile test, shear test, torsion te...
New skin alloys are being developed that are both damage tolerant and strong in compression. At the ...
This paper deals with the experimental and numerical evaluation of the buckling behaviour and ultima...
The Channel steel is a common material that is used in the construction structure. This material is...
The stiffened steel panel will experienced high stress when the deck and bottom shell of ship hulls...
This research aims to study the ultimate limit state (ULS) behaviour of stiffened panel under longit...
The results obtained on two closed structural boxes composed by four graphite-epoxy curved stringer-...
The work presented in this thesis focuses on the behaviour of compressed stiffeners in steel connect...
Buckling and postbuckling of plates and stiffened panels are considered. Computational models for di...
ABSTRACTThis paper concentrated on the ultimate uniaxial compressive strength of stiffened panel wit...
Stiffened composite panels are primary structural components in ship, aircraft and aerospace vehicle...
The results of 8 tests on panels under axial compression until collapse are presented. The panels ar...
of the Institute of Aerophysics for providing the opportunity of carrying out this investigation. Th...
An analysis for determining the effects of eccentricities and lateral pressure on the design of stif...
The aim of this research was to find design data for the stiffened plywood panels supplied by the Fl...
As the steel is tested for all types of tests viz, compressive, tensile test, shear test, torsion te...
New skin alloys are being developed that are both damage tolerant and strong in compression. At the ...
This paper deals with the experimental and numerical evaluation of the buckling behaviour and ultima...
The Channel steel is a common material that is used in the construction structure. This material is...
The stiffened steel panel will experienced high stress when the deck and bottom shell of ship hulls...
This research aims to study the ultimate limit state (ULS) behaviour of stiffened panel under longit...
The results obtained on two closed structural boxes composed by four graphite-epoxy curved stringer-...
The work presented in this thesis focuses on the behaviour of compressed stiffeners in steel connect...
Buckling and postbuckling of plates and stiffened panels are considered. Computational models for di...
ABSTRACTThis paper concentrated on the ultimate uniaxial compressive strength of stiffened panel wit...
Stiffened composite panels are primary structural components in ship, aircraft and aerospace vehicle...