Structural Assessment of FML Aerostructures with Integrated Electromagnetic Features


== Abstract ==

A substantial contribution to reduce the aerodynamic drag and consequent CO2 and
NOx emissions is to integrate communication antennas in the aircraft structure. This paper
presents a GLARE fuselage panel design for an integrated VHF slot antenna and discusses the
results of a mechanical experimental campaign on a structural element level, in quasi-static
tensile conditions. The tested specimens showed small variability in terms of stiffness and
strength (typical for GLARE), little dependence on the ambient conditions, damage presence,
and layup configurations and good agreement with early numerical simulations. In addition,
stiffness and strength predictions, based on empirically found design values seem to correlate
well with the found test values

== Full document ==
<pdf>Media:Draft_Content_390987823-P_IDC5_42-2779-document.pdf</pdf>


== References ==

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