During the preliminary design of stiffened panels, the stability behaviour is critical and both buckling modes, global and local, have to be considered in order to avoid panel configurations in which the minimum stiffness of the stringers is not achieved. In the present work, a new simple computational model is presented that computes the critical column buckling load of an omega-stringer-stiffened panel with periodic boundary conditions. This is achieved by obtaining the effective stiffness properties for an equivalent composite column. The model is able to predict column buckling conservatively as numerical studies show and can easily be used, e.g. as a constraint for optimization studies
This paper presents a semi-analytical method for the buckling analysis of composite panels reinforce...
This paper presents a semi-analytical method for the buckling analysis of composite panels reinforce...
This paper presents a semi-analytical method for the buckling analysis of composite panels reinforce...
During the preliminary design of stiffened panels, the stability behaviour is critical and both buck...
During the preliminary design of stiffened panels, the stability behaviour is critical and both buck...
During the preliminary design of stiffened panels, the stability behaviour is critical and both buck...
During the preliminary design of stiffened panels, the stability behaviour is critical and both buck...
During the preliminary design of stiffened panels, the stability behaviour is critical and both buck...
During the preliminary design of stiffened panels, the stability behaviour is critical and both buck...
During the preliminary design of stiffened panels, the stability behaviour is critical and both buck...
During the preliminary design of stiffened panels, the stability behaviour is critical and both buck...
For the preliminary structural design of aircraft, spacecraft and marine vessels, computationally ef...
The stability behavior is critical for thin-walled composite structures. This type of structures is ...
It is well known [1] that non-closely stiffened panels can have considerable postbuckling reserve st...
This paper presents a semi-analytical method for the buckling analysis of composite panels reinforce...
This paper presents a semi-analytical method for the buckling analysis of composite panels reinforce...
This paper presents a semi-analytical method for the buckling analysis of composite panels reinforce...
This paper presents a semi-analytical method for the buckling analysis of composite panels reinforce...
During the preliminary design of stiffened panels, the stability behaviour is critical and both buck...
During the preliminary design of stiffened panels, the stability behaviour is critical and both buck...
During the preliminary design of stiffened panels, the stability behaviour is critical and both buck...
During the preliminary design of stiffened panels, the stability behaviour is critical and both buck...
During the preliminary design of stiffened panels, the stability behaviour is critical and both buck...
During the preliminary design of stiffened panels, the stability behaviour is critical and both buck...
During the preliminary design of stiffened panels, the stability behaviour is critical and both buck...
During the preliminary design of stiffened panels, the stability behaviour is critical and both buck...
For the preliminary structural design of aircraft, spacecraft and marine vessels, computationally ef...
The stability behavior is critical for thin-walled composite structures. This type of structures is ...
It is well known [1] that non-closely stiffened panels can have considerable postbuckling reserve st...
This paper presents a semi-analytical method for the buckling analysis of composite panels reinforce...
This paper presents a semi-analytical method for the buckling analysis of composite panels reinforce...
This paper presents a semi-analytical method for the buckling analysis of composite panels reinforce...
This paper presents a semi-analytical method for the buckling analysis of composite panels reinforce...