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Browsing by Supervisor "Zhang, Xiang"

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Modelling and predicting fatigue crack growth behaviour in weld induced residual stress fields

Servetti, Guido (Cranfield University, 2011-01)

In the last few decades, new design concepts and manufacture processes have been developed in order to reduce the maintenance and manufacturing costs, and structural weight of aircraft components. The integral metallic ...
Numerical modelling of composite laminates with through-thickness-reinforcements

Grassi, Marcello (Cranfield University, 2004-03)

The main objective of the present research study was to develop numerical models to investigate the mechanical properties and effectiveness of z-fibre reinforced laminates. A survey of relevant literature on through-thickness ...
Numerical modelling of through-thickness reinforced structural joints

Bianchi, Francesco (Cranfield University, 2012-06)

The main objective of this research study was to develop numerical models to analyse the mechanical and fracture properties of through-thickness reinforced (TTR) structural joints. The development of numerical tools was ...
Ply clustering effect on composite laminates under low-velocity impact using FEA

Liu, Hongquan (Cranfield University, 2012-01)

With the development of the design and manufacture technology, composite materials are widely used in the aeronautical industry. But, one of the main concerns which affects the application of composites is foreign object ...
Predicting fatigue crack growth life in integral metallic skin-stringer panels

Shi, Zhijun (Cranfield University, 2012-01)

During the past few years, in comparison to traditional riveted structures, integral metallic skin stringer structures have played more and more important roles in aircraft design due to the fact they are economical and ...

Browsing by Supervisor "Zhang, Xiang"

Browsing by Supervisor "Zhang, Xiang"

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