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== Abstract == | == Abstract == | ||
| − | The objective of this paper is to describe the numerical simulation of the transition | + | The objective of this paper is to describe the numerical simulation of the transition zones in the multifunctional fuselage panel design to integrate a VHF (Very High Frequency) antenna. The panel is made of GLARE (Glass Laminate Aluminium Reinforced Epoxy) with a central window of GFRP (Glass Fibre Reinforced Polymer). The structural analyses of the transition GLARE/GFRP is presented along with its experimental validation. The numerical simulations showed a very high level of correlation with the experimental tests, both in the longitudinal load vs displacement curves and deformations captured with strain gauges and DIC (Digital Image Correlations). |
| − | zones in the multifunctional fuselage panel design to integrate a VHF (Very High Frequency) antenna. The panel is made of GLARE (Glass Laminate Aluminium Reinforced Epoxy) with a central window of GFRP (Glass Fibre Reinforced Polymer). The structural analyses of the transition GLARE/GFRP is presented along with its experimental validation. The numerical simulations showed a very high level of correlation with the experimental tests, both in the longitudinal load vs displacement curves and deformations captured with strain gauges and DIC (Digital Image Correlations). | + | |
== Full document == | == Full document == | ||
| − | <pdf>Media: | + | <pdf>Media:Turon_et_al_2021a_7445_P_IDC5_32.pdf</pdf> |
| + | |||
| + | == References == | ||
| + | |||
| + | [1] Rastellini F. and Oller S. and Salomón O. and Oñate, E. Composite materials non-linear modelling for long fibre-reinforced laminates continuum basis, computational aspect and validations. Computers and Structures. (2008) 86:879-896. | ||
| + | |||
| + | [2] Car E. and Oller S. and Oñate, E. An anisotropic elastoplastic constitutive model for large strain analysis of fiber reinforced composite materials. Computer Methods in Applied Mechanics and Engineering. (2000) 185:245-277. | ||
| + | |||
| + | [3] Martinez X. and Oller S. Numerical simulation of matrix reinforced composite materials subjected to compression loads. Archives of computational methods in engineering. (2009) 16:357-397. | ||
| + | |||
| + | [4] Francesc Turon, Fermin Otero And Xavier Martinez. Structural Analyses Of Orthogrid Fuselage Panel For Integrated Ku-Band Satcom Antenna – Emus 2019" | ||
Latest revision as of 14:26, 1 March 2021
Abstract
The objective of this paper is to describe the numerical simulation of the transition zones in the multifunctional fuselage panel design to integrate a VHF (Very High Frequency) antenna. The panel is made of GLARE (Glass Laminate Aluminium Reinforced Epoxy) with a central window of GFRP (Glass Fibre Reinforced Polymer). The structural analyses of the transition GLARE/GFRP is presented along with its experimental validation. The numerical simulations showed a very high level of correlation with the experimental tests, both in the longitudinal load vs displacement curves and deformations captured with strain gauges and DIC (Digital Image Correlations).
Full document
References
[1] Rastellini F. and Oller S. and Salomón O. and Oñate, E. Composite materials non-linear modelling for long fibre-reinforced laminates continuum basis, computational aspect and validations. Computers and Structures. (2008) 86:879-896.
[2] Car E. and Oller S. and Oñate, E. An anisotropic elastoplastic constitutive model for large strain analysis of fiber reinforced composite materials. Computer Methods in Applied Mechanics and Engineering. (2000) 185:245-277.
[3] Martinez X. and Oller S. Numerical simulation of matrix reinforced composite materials subjected to compression loads. Archives of computational methods in engineering. (2009) 16:357-397.
[4] Francesc Turon, Fermin Otero And Xavier Martinez. Structural Analyses Of Orthogrid Fuselage Panel For Integrated Ku-Band Satcom Antenna – Emus 2019"
Document information
Published on 15/02/21
Submitted on 15/02/21
DOI: 10.23967/emus.2020.002
Licence: CC BY-NC-SA license
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