Repairing of the cracks by fiber metal laminates (FMLs) was first done by some aeronautical laboratories in early 1970s. In this study, experimental investigations were done on the effect of repairing the center-cracked aluminum plates using the FML patches. The repairing processes were conducted to characterize the response of the repaired structures to tensile tests. The composite patches wer...

Sixth-generation wireless communication (6G) will be an integrated architecture of "space, air, ground and sea". One the most difficult part this is underwater information acquisition which need to transmitt cross interface between water air.In senario, ocean things (OoT) play important role, because it can serve as a hub connecting Internet (IoT) (IoUT). OoT device not only collect data throug...

The competitive and open market nature demands different vendors to collaborate during the product life cycle and to reduce the product’s time to market. In this paper, we propose an infrastructure to enable the concurrent collaboration of heterogeneous Computer Aided tools for concurrent engineering aspect X (CAX) at the feature level using a Service Oriented Architecture (SOA) approach. A Fea...

An issue of concern in aging aircraft is the growth of multiple cracks emanating from a row of fastener holes, typically in a pressurized aircraft fuselage lap splice. This multisite damage (MSB), or widespread fatigue damage, if allowed to progress, can suddenly become catastrophic. The understanding of the failure behavior dictates the level of compromise between safety and economy. The compl...

Although most of the basic animal body plans are supported by hydrostatic skeletons consisting of fluid maintained at constant volume, studies on how animals have solved biomechanical scaling dilemmas during evolution of large body size have emphasized cases where skeletons are formed by rigid solids. Larvae of gastropod molluscs swim using ciliated velar lobes supported by a constant volume hy...

The compound strip method (CSM) for plates is an expansion of the finite strip method (FSM) and was developed to incorporate the effects of the support elements in the analysis of linear elastic plate systems. In this paper the CSM is further expanded to analyze structures such as stiffened plates under loads in the plane of the plate or the so called plane-stress condition. Examples of these t...

The circumferential profile of cylinder, as a classic shape, has been widely adopted in single-layer latticed shells. Previous research into these structures primarily concentrated on their buckling behavior. In this work, novel two-way aluminum alloy cable-stiffened shell is proposed to explore shape optimization procedure such structure. addition, the behavior optimized and cylindrical shells...