A closed form solution of the Stress Intensity Factor (SIF) for stiffened flat sheets, typically used in aircraft construction, in Multiple Site Damage (MSD) conditions, has been developed. The well-known theory of complex variable functions has been used, through the application of functions specifically developed for the case of cracks equally spaced and of equal length. Moreover, the superposition principle has been applied to evaluate the compression loads transmitted by the stringers through the rivets, by imposing the equilibrium on the crack free surfaces and the compatibility of displacements between sheet and stringers at the rivets location. The results have been compared with solutions available in the literature, obtained by com...
The problem of cracked plates stiffened by three-dimensional stringers is investigated using transmi...
Tensile sheets with symmetrically placed cracks on opposite edges are studied using the displacement...
A model for crack growth prediction in stiffened sheets and joints with multiple cracks is presented...
A closed form solution of the Stress Intensity Factor (SIF) for stiffened flat sheets, typically use...
The analysis of stiffened panel structures containing multiple site damage is addressed through the ...
A theoretical formulation is presented for determining stress intensity factors for cracks in an inf...
This paper presents a stress intensity factor solution for cracks located in panels reinforced with ...
This paper presents a stress intensity factor solution for cracks located in panels reinforced with ...
Previous work on both continuously attached and discretely attached stiffeners and patches is review...
Multiple site damage (MSD) is a type of cracking that may be found in aging airplanes which can adve...
Multi-site damage need to be addressed and evaluated in order to assess the integrity of aging aircr...
In the face of enormous costs of developing new aircraft, high fuel prices, increasingly demanding e...
peer reviewedLong-strip elements are plentiful in ai rcraft structure; they represent one type of MS...
Report prepared Jul 1975Available from British Library Document Supply Centre- DSC:8717.806(RAE-TR--...
Mathematical models are formulated for the stress analysis of a patch bonded over a crack in a large...
The problem of cracked plates stiffened by three-dimensional stringers is investigated using transmi...
Tensile sheets with symmetrically placed cracks on opposite edges are studied using the displacement...
A model for crack growth prediction in stiffened sheets and joints with multiple cracks is presented...
A closed form solution of the Stress Intensity Factor (SIF) for stiffened flat sheets, typically use...
The analysis of stiffened panel structures containing multiple site damage is addressed through the ...
A theoretical formulation is presented for determining stress intensity factors for cracks in an inf...
This paper presents a stress intensity factor solution for cracks located in panels reinforced with ...
This paper presents a stress intensity factor solution for cracks located in panels reinforced with ...
Previous work on both continuously attached and discretely attached stiffeners and patches is review...
Multiple site damage (MSD) is a type of cracking that may be found in aging airplanes which can adve...
Multi-site damage need to be addressed and evaluated in order to assess the integrity of aging aircr...
In the face of enormous costs of developing new aircraft, high fuel prices, increasingly demanding e...
peer reviewedLong-strip elements are plentiful in ai rcraft structure; they represent one type of MS...
Report prepared Jul 1975Available from British Library Document Supply Centre- DSC:8717.806(RAE-TR--...
Mathematical models are formulated for the stress analysis of a patch bonded over a crack in a large...
The problem of cracked plates stiffened by three-dimensional stringers is investigated using transmi...
Tensile sheets with symmetrically placed cracks on opposite edges are studied using the displacement...
A model for crack growth prediction in stiffened sheets and joints with multiple cracks is presented...