Study on the influence of localised thermal load on collapse strength of stiffened panels under longitudinal compression

2021 ◽  
Vol 239 ◽  
pp. 112364
Author(s):  
Ming Cai Xu ◽  
Zhao Jun Song ◽  
Jin Pan ◽  
Tao Wang
1972 ◽  
Vol 23 (1) ◽  
pp. 24-40 ◽  
Author(s):  
F W Williams ◽  
W H Wittrick

SummaryIn previous papers the basis of a matrix approach to the initial buckling or vibration of prismatic structures consisting of a series of thin flat rectangular plates rigidly connected together along their longitudinal edges has been developed. The present paper provides numerical results for the buckling, under uniform longitudinal compression, of a series of panels with unflanged or flanged integral stiffeners, or with Z-section stiffeners; the results are compared with those obtained by other methods and with published results, including an appropriate Royal Aeronautical Society Structures Data Sheet. It was found that considerable inaccuracies can arise from the usual methods of analysis and the authors believe that these justify the use of computer programmes, such as the ones used to obtain the results of this paper, at least at the final design stage.


Author(s):  
Ming Cai Xu ◽  
C. Guedes Soares

The results of five tests on narrow stiffened panels under axial compression until collapse and beyond are presented to investigate the collapse behaviors of stiffened panels. Tension tests were used to evaluate the material properties of the stiffened panels. The tests were made on panels with two half bays plus one full bay in the longitudinal direction. Initial loading cycles were used to eliminate the residual stresses of the stiffener panels. The strain gauges were set on the plates and the stiffeners to record the strain histories. The displacement load relationship was established. The collapse behavior, modes of failure and load-carrying capacity of the stiffened panels are investigated with the experiment.


Author(s):  
Mingcai Xu ◽  
C. Guedes Soares

The results of four tests on narrow stiffened panels under axial compression until collapse and beyond are presented to investigate the ultimate strength of stiffened panels. Tension tests are used to evaluate the material properties of the stiffened panels. The tests are made on panels with two half bays plus one full bay in the longitudinal direction. Initial loading cycles were used to relief the residual stresses of the stiffener panels. The strain gauges are set on the plates and stiffeners to record the distribution of strain. The displacement load relationship is established. The ultimate strength behavior, modes of failure and load-carrying capacity of the stiffened panels are investigated with the experiment.


2019 ◽  
Vol 11 (10) ◽  
pp. 168781401988476
Author(s):  
Jin Pan ◽  
Na Li ◽  
Zhao Jun Song ◽  
Ming Cai Xu

A series of stiffened panels with different dimensions and types of stiffener are simulated under longitudinal compression in finite element code ANSYS. Two bays/spans model with periodic boundary condition is adopted to consider the influence of neighbouring members. The stiffened panel adopted in the finite element mode is generally cut from the deck or bottom of a ship hull girder, and thus, the constraint on their edges depends to some extent on the relative structural response of the adjacent members. Hence, to understand the effects of constraint condition on the collapse behaviour, an extensive parametric study is carried out, employing a wide geometrical range for bulk carrier and very large crude carrier. Moreover, considering various collapse modes, the load-carrying capacities of the stiffened panels are also investigated for various stiffener types. It is found that the biaxial stress state caused by longitudinal constraint could increase or decrease the load-carrying capacity of the stiffened panel, which depends on the collapse mode and should be noticed. The transverse constraint on the longitudinal edges could cause biaxial stress state, which might increase or decrease the load-carrying capacity of the stiffened panel, which depends on the collapse modes.


Author(s):  
Malgorzata Witkowska ◽  
C. Guedes Soares

In this study the behaviour and ultimate strength of damaged stiffened panels is investigated. The damage is in a form of local imperfection and represents a dent that could be caused by a fall or strike of an object. The model used is a panel made of five plates joined transversally with four longitudinal flat-bar stiffeners. Finite element non-linear analysis of panels having different geometrical properties is carried out. The influence of several parameters has been studied in order to establish their interaction with the presence of the local dent. It has been found that stiffened panels present quite good performance while subjected to the local damage, however, depending on geometrical characteristics, a problem of stiffener deformations may occur, significantly lowering the ultimate strength.


1974 ◽  
Vol 25 (3) ◽  
pp. 165-179 ◽  
Author(s):  
R J Plank ◽  
F W Williams

SummaryPrevious papers by the authors and others have developed exact methods for computing the critical buckling loads of prismatic assemblies of rigidly interconnected thin flat rectangular plates. The plates may be isotropic or anisotropic and can carry uniform in-plane shear stresses and transverse stresses in addition to a longitudinal stress which varies linearly over the cross section but is longitudinally invariant. Published results obtained using these methods have only covered a few of the types of structure and loading which are of interest. This paper presents results which complement those already published. For instance, interaction curves are given for common types of panel in combined in-plane shear and longitudinal compression and bending. About half of these curves are nearly parabolic while some others differ greatly from the parabola, which errs on the safe side for all the results presented. Other results cover critical loads other than the lowest, panels with bulb flat stiffeners, as used for bridge decks, and the effects of assumptions usually made when idealising real panels before computation.


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