An analysis was performed to evaluate the stress distribution in composite pin loaded joints. The analysis involves specification of displacement expressions in the form of a trigonometric series that satisfy the boundary conditions for the contact region in terms of a set of undetermined coefficients. Based on this assumed distribution, the Lekhnitskii complex variable approach is used to obtain the stress functions needed to evaluate the contact stresses within the joint. Unknown coefficients in the displacement expression were obtained by assuming coulomb friction within the contact region and evaluating the displacement at discrete points within this region. Material properties of carbon fiber reinforced plastic laminates were used for ...
AbstractThe effects of tangential friction at pin—hole interfaces are appropriately modelled for the...
Abstract—General solutions for determining the stress field around triangular hole in infinite ortho...
A parametric study of the stress distribution in the composite plates is undertaken to show the effe...
Pin-loaded holes commonly occur in engineering structures. However, accurate analysis of such holes ...
The stress distribution round a pin-loaded hole in an elastically ortho-tropic or isotropic plate is...
Pin-loaded holes commonly occur in engineering structures. However, accurate analysis of such holes ...
Results of a linear elastic, plane stress finite element investigation of the stress distribution ar...
Space structures are built up using fiber composite material, due to its lightweight. Holes of diffe...
Fiber reinforced composites have emerged as high performance materials for a variety of engineering ...
Mechanical joints in composites can be tailored to achieve improved peiformance and better life by a...
Mechanical joints in composites can be tailored to achieve improved peiformance and better life by a...
Mechanical joints in composites can be tailored to achieve improved performance and better life by a...
Mechanical joints in composites can be tailored to achieve improved performance and better life by a...
The effects of tangential friction at pin—hole interfaces are appropriately modelled for the analysi...
The effects of tangential friction at pin—hole interfaces are appropriately modelled for the analysi...
AbstractThe effects of tangential friction at pin—hole interfaces are appropriately modelled for the...
Abstract—General solutions for determining the stress field around triangular hole in infinite ortho...
A parametric study of the stress distribution in the composite plates is undertaken to show the effe...
Pin-loaded holes commonly occur in engineering structures. However, accurate analysis of such holes ...
The stress distribution round a pin-loaded hole in an elastically ortho-tropic or isotropic plate is...
Pin-loaded holes commonly occur in engineering structures. However, accurate analysis of such holes ...
Results of a linear elastic, plane stress finite element investigation of the stress distribution ar...
Space structures are built up using fiber composite material, due to its lightweight. Holes of diffe...
Fiber reinforced composites have emerged as high performance materials for a variety of engineering ...
Mechanical joints in composites can be tailored to achieve improved peiformance and better life by a...
Mechanical joints in composites can be tailored to achieve improved peiformance and better life by a...
Mechanical joints in composites can be tailored to achieve improved performance and better life by a...
Mechanical joints in composites can be tailored to achieve improved performance and better life by a...
The effects of tangential friction at pin—hole interfaces are appropriately modelled for the analysi...
The effects of tangential friction at pin—hole interfaces are appropriately modelled for the analysi...
AbstractThe effects of tangential friction at pin—hole interfaces are appropriately modelled for the...
Abstract—General solutions for determining the stress field around triangular hole in infinite ortho...
A parametric study of the stress distribution in the composite plates is undertaken to show the effe...