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FML full scale aeronautic panel under multiaxial fatigue: Experimental test and DBEM Simulation
Engineering Fracture Mechanics, 2011Abstract This paper concerns the numerical and experimental characterization of the static and fatigue strength of a flat stiffened panel, designed as a Fibre Metal Laminate (FML) and made of aluminium alloy and Fibre Glass FRP. The panel is full scale and was tested under both static and fatigue bi-axial loads, applied by means of an in house ...
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Assessment of damage containment features of a full-scale PRSEUS fuselage panel
Composite Structures, 2014Abstract The most recent generation of integrally stitched composite technology is the Pultruded Rod Stitched Efficient Unitized Structure (PRSEUS) concept, which shows promise in enhancing structural integrity of aircraft and aerospace structures. An assessment of damage-containment capabilities of the PRSEUS concept for a full-scale fuselage panel ...
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