Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76867/1/AIAA-2004-2051-840.pd
The panel analysis and optimization code VICONOPT, based on exact strip theory, is utilized to inves...
A computationally efficient two-level design methodology is developed for the optimization of stiffe...
In this study, an analytical solution has been developed for the elastic buckling analysis of stiffe...
New skin alloys are being developed that are both damage tolerant and strong in compression. At the ...
Stiffened panels with curved stiffeners have shown a potential for structural tailoring of metallic ...
Design of robust aircraft structure requires consideration of the load-carrying capability with larg...
This paper investigates the weight minimization of stiffened panels simultaneously optimizing sizing...
Stiffened panels are widely used in aircraft structures such as wing covers, fuselages, control surf...
This paper describes the analysis and the minimum weight optimisation of a fuselage composite stiffe...
It is well known [1] that non-closely stiffened panels can have considerable postbuckling reserve st...
The efficient, industrially used, linear elastic preliminary design software VICONOPT is employed to...
In modern conceptual/preliminary design of aerospace vehicles it is common for a large number of con...
In this thesis, an automated buckling check method has been developed and validated for thin plated ...
AbstractModern aircraft wings are thin-walled structures composed of ribs, spars and stiffened panel...
A compressively-loaded stiffened panel has been designed with post-buckling reserve of strength in i...
The panel analysis and optimization code VICONOPT, based on exact strip theory, is utilized to inves...
A computationally efficient two-level design methodology is developed for the optimization of stiffe...
In this study, an analytical solution has been developed for the elastic buckling analysis of stiffe...
New skin alloys are being developed that are both damage tolerant and strong in compression. At the ...
Stiffened panels with curved stiffeners have shown a potential for structural tailoring of metallic ...
Design of robust aircraft structure requires consideration of the load-carrying capability with larg...
This paper investigates the weight minimization of stiffened panels simultaneously optimizing sizing...
Stiffened panels are widely used in aircraft structures such as wing covers, fuselages, control surf...
This paper describes the analysis and the minimum weight optimisation of a fuselage composite stiffe...
It is well known [1] that non-closely stiffened panels can have considerable postbuckling reserve st...
The efficient, industrially used, linear elastic preliminary design software VICONOPT is employed to...
In modern conceptual/preliminary design of aerospace vehicles it is common for a large number of con...
In this thesis, an automated buckling check method has been developed and validated for thin plated ...
AbstractModern aircraft wings are thin-walled structures composed of ribs, spars and stiffened panel...
A compressively-loaded stiffened panel has been designed with post-buckling reserve of strength in i...
The panel analysis and optimization code VICONOPT, based on exact strip theory, is utilized to inves...
A computationally efficient two-level design methodology is developed for the optimization of stiffe...
In this study, an analytical solution has been developed for the elastic buckling analysis of stiffe...
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