Modern lightweight structures commonly use stiffeners of constant cross section to increase the stability of thin shells. This paper introduces a particular ΩΩ stringer with variable cross section, allowing an increase of local skin buckling load, through an effective partitioning of the skin fields. The present work contains a methodology to develop a feasible design for stiffened shells. Parametric studies including criteria like stability, strength and damage tolerance, are performed. Additionally, a static compression experiment is conducted. Considering actual sizing criteria it can be shown that the introduced type of stringer leads to improved load carrying capacity through weight quotients
A computationally efficient two-level design methodology is developed for the optimization of stiffe...
In this paper a buckling design rule for stringer stiffened curved CFRP panels subjected to combined...
Local buckling of elements supporting the compressed power panels of aircraft structures, stringer, ...
It is well known [1] that non-closely stiffened panels can have considerable postbuckling reserve st...
A methodology is presented to investigate and improve the strength and damage tolerance of stiffened...
The buckling strength of conical shells subjected to axial compression may be increased by means of ...
New skin alloys are being developed that are both damage tolerant and strong in compression. At the ...
A methodology is presented to investigate and improve the strength and damage tolerance of stiffened...
Aeronautical composite stiffened structures have the capability to carry loads deep into postbucklin...
Aeronautical composite stiffened structures have the capability to carry loads deep into postbucklin...
In this contribution, results obtained from buckling and post buckling tests of stringer stiffened p...
This paper presents FEM calculations using the program package MSC/NASTRAN for linear buckling analy...
The results of an experimental investigation of two stringer-stiffened shells and of two ring- and s...
Aeronautical composite stiffened structures have the capability to carry loads deep into postbucklin...
Low cost and less weight are the two primary objectives of any Aircraft structure. Efficient design ...
A computationally efficient two-level design methodology is developed for the optimization of stiffe...
In this paper a buckling design rule for stringer stiffened curved CFRP panels subjected to combined...
Local buckling of elements supporting the compressed power panels of aircraft structures, stringer, ...
It is well known [1] that non-closely stiffened panels can have considerable postbuckling reserve st...
A methodology is presented to investigate and improve the strength and damage tolerance of stiffened...
The buckling strength of conical shells subjected to axial compression may be increased by means of ...
New skin alloys are being developed that are both damage tolerant and strong in compression. At the ...
A methodology is presented to investigate and improve the strength and damage tolerance of stiffened...
Aeronautical composite stiffened structures have the capability to carry loads deep into postbucklin...
Aeronautical composite stiffened structures have the capability to carry loads deep into postbucklin...
In this contribution, results obtained from buckling and post buckling tests of stringer stiffened p...
This paper presents FEM calculations using the program package MSC/NASTRAN for linear buckling analy...
The results of an experimental investigation of two stringer-stiffened shells and of two ring- and s...
Aeronautical composite stiffened structures have the capability to carry loads deep into postbucklin...
Low cost and less weight are the two primary objectives of any Aircraft structure. Efficient design ...
A computationally efficient two-level design methodology is developed for the optimization of stiffe...
In this paper a buckling design rule for stringer stiffened curved CFRP panels subjected to combined...
Local buckling of elements supporting the compressed power panels of aircraft structures, stringer, ...