About the Project
The project deals with semi-analytical and numerical study of dynamic response in composite beams with a particular through thickness architecture (lay-up) subjected to low and high amplitude pulse loads of low and high durations. The cross section of the typical beam varies along the length and is selected to be a combination of the standard NREL S818, S825 and S826 airfoils twisted at a predefined angle to maximise lift. All regimes of response viz. impulsive, dynamic and quasi-static are ought to be considered. In all cases the monolithic counterpart is also analysed as a benchmark.
The aim of the project is thus to establish a relationship between the features that determine the pulse load uniquely and the response outputs.
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