De-Freitas et al 2020a - Revision history

Scipediacontent at 16:38, 17 February 2021

2021-02-17T16:38:34Z

Scipediacontent at 08:32, 16 February 2021

2021-02-16T08:32:54Z

Scipediacontent: Scipediacontent moved page Draft Content 390987823 to De-Freitas et al 2020a

2021-02-16T08:25:55Z

Scipediacontent moved page Draft Content 390987823 to De-Freitas et al 2020a

Scipediacontent: Created page with " == Abstract == A substantial contribution to reduce the aerodynamic drag and consequent CO2 and NOx emissions is to integrate communication antennas in the aircraft structur..."

2021-02-16T08:25:53Z

Created page with " == Abstract == A substantial contribution to reduce the aerodynamic drag and consequent CO2 and NOx emissions is to integrate communication antennas in the aircraft structur..."

New page

== 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 ==

[1] J. Rotgerink, C. Heuts, J. Verpoorte and C. van Hengel, "VHF antenna integrated into a classical fibre metal laminate fuselage panel.," in ''European Conference on Multifunctional Structures'', Barcelona, 2020.

[2] G. Wu and J. Yang, "The Mechanical Behavior of GLARE Laminates for Aircraft Structures," ''Journal of the Minerals'', ''Metals and Materials Society'', pp. 72-79, 2005.

[3] R. Alderliesten and J. Homan, "Fatigue and damage tolerance issues of Glare in aircraft structures.," ''International Journal of Fatigue'', vol. 28, pp. 1116-1123, 2006.

[4] R. Citarella, E. Armentani, R. Sepe and F. Caputo, "FEM Simulation of a FML Full Scale Aeronautic Panel Undergoing Static Load," ''Industrial Engineering & Management'', vol. 3, no. 1, 2014.

[5] Fokker Aerostructures, "TH3-305 - Material design values and mechanical properties of standard GLARE," Papendrecht, 2006.

[6] M. Hagenbeek, "Characterisation of Fibre Metal Laminates under Thermo-mechanical Loadings," TU Delft, Delft, 2005.

[7] University of Bristol, "Certification for Design - Reshaping the Testing Pyramid," UK Research and innovation, Swindon, 2020.

[8] F. Turon, F. Otero and X. Martinez, "Structural analyses of GLARE-GFRP transition for integrated VHF antenna on a fuselage panel," in ''European Conference on Multifunctional Structures'', Barcelona, 2020.

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 == Full document ==
-<pdf>Media:Draft_Content_390987823-P_IDC5_42-2779-document.pdf</pdf>
+<pdf>Media:De-Freitas_et_al_2020a_2009_P_IDC5_42.pdf</pdf>
-−
 == References ==

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 == Abstract ==
-A substantial contribution to reduce the aerodynamic drag and consequent CO2 and
+A substantial contribution to reduce the aerodynamic drag and consequent CO<sub>2</sub> and NO<sub>x</sub> 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
-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 ==

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