Add to ORKGAn approach to buckling resistant design of general grid stiffened flat plates based on smeared stiffener theory for combined inplane loading is discussed. Some results from parametric studies performed to assess the validity of smeared stiffener for practical stiffener configurations and to illustrate the benefits of different stiffening concepts are given. Details of a design study are discussed where the present analysis method is used to design a grid stiffened panel for a fuselage application and verified using a finite element analysis results
Adhesive junctions or co-infusion of skin and stiffeners represent efficient manufacturing processes...
Stiffened thin panels are very common and important structural elements in aerospace structures beca...
Modern aircraft wings are thin-walled structures composed of ribs, spars and stiffened panels, where...
A design strategy for optimal design of composite grid-stiffened panels subjected to global and loca...
Continuous filament grid-stiffened structure is a stiffening concept that combines structural effici...
With the goal of tailorability in mind, the in-plane stiffness characteristics of a particular grid ...
The design and analysis of stiffened composite panel that is representative of the fuselage structur...
A stiffened composite panel has been designed that is representative of the fuselage structure of ex...
Geodesically stiffened structures are very efficient in carrying combined bending, torsion, and pres...
Grid-stiffened composite structures, where the skin is stiffened by a lattice of stiffeners, not onl...
This paper describes the analysis and the minimum weight optimisation of a fuselage composite stiffe...
For past decades devolopment of composite material had brought tremendous change in AirFrames and M...
The results of an analytical and experimental investigation of the failure of composite is tiffener ...
An exact linear analysis method is presented for predicting buckling of structures with arbitrary un...
AbstractModern aircraft wings are thin-walled structures composed of ribs, spars and stiffened panel...
Adhesive junctions or co-infusion of skin and stiffeners represent efficient manufacturing processes...
Stiffened thin panels are very common and important structural elements in aerospace structures beca...
Modern aircraft wings are thin-walled structures composed of ribs, spars and stiffened panels, where...
A design strategy for optimal design of composite grid-stiffened panels subjected to global and loca...
Continuous filament grid-stiffened structure is a stiffening concept that combines structural effici...
With the goal of tailorability in mind, the in-plane stiffness characteristics of a particular grid ...
The design and analysis of stiffened composite panel that is representative of the fuselage structur...
A stiffened composite panel has been designed that is representative of the fuselage structure of ex...
Geodesically stiffened structures are very efficient in carrying combined bending, torsion, and pres...
Grid-stiffened composite structures, where the skin is stiffened by a lattice of stiffeners, not onl...
This paper describes the analysis and the minimum weight optimisation of a fuselage composite stiffe...
For past decades devolopment of composite material had brought tremendous change in AirFrames and M...
The results of an analytical and experimental investigation of the failure of composite is tiffener ...
An exact linear analysis method is presented for predicting buckling of structures with arbitrary un...
AbstractModern aircraft wings are thin-walled structures composed of ribs, spars and stiffened panel...
Adhesive junctions or co-infusion of skin and stiffeners represent efficient manufacturing processes...
Stiffened thin panels are very common and important structural elements in aerospace structures beca...
Modern aircraft wings are thin-walled structures composed of ribs, spars and stiffened panels, where...