Composite Cylindrical Shell Buckling: Simulation & Experimental Correlation

Guidelines dating back 50 years, NASA SP-8007, are employed today in the design of thin-walled launch vehicle structures. Due to advances in materials, structural designs, and manufacturing techniques since the publication of SP-8007, the development of new knockdown factors for contemporary launch vehicle structures is an ongoing subject of...

Effect of welding induced residual stresses on compressive failure load of column structures

Structural members carrying dominantly compressive forces are present in many types of structure. These members are referred to as columns and are frequently present in for example lifting appliances and offshore structures. Whether or not a column consists of longitudinally welded subsections is relevant for its mechanical performance in...

A numerical study of delamination propagation in post-buckled single stringer compression specimens using the virtual crack closure technique

To enable weight reduction of skin stiffened structures in aerospace applications they can be loaded in the post-buckling regime during service. However, to do this safely the fatigue delamination growth behaviour of post-buckled skin stiffened structures must be well understood. To this end, skin-stiffener separation of single stringer...