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Revision as of 08:56, 4 March 2021
Abstract
This paper outlines aspects, outcome and prospects of full integration of antennas into structural elements of aircraft, from a structural design perspective.
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References
[1] Yuri E. Konter†, Charly Heuts and Cees van Hengel “Exploration Of Radiating Aerostructures Ultimate Antenna And Structure Integration” – EMuS 2019, June, BARCELONA, Spain
[2] Hinrichsen, J.: “The Material Down-selection Process for A3XX”; Keynote Address to the “19th European Conference on Materials for Aerospace Applications”, Confederation of European Aerospace Societies (CEAS), Munich, Germany Dec. 6th – 8th, 2000.
[3] Dr.-Ing. Thomas Beumler,: “Airbus Fiber Metal Laminate Structures – from Laboratory to Application”, Lecture to RAeS Hamburg Branch, 29 October 2009, https://www.fzt.haw-hamburg.de//pers/Scholz/dglr/hh/text_2009_10_29_Fiber_Metal_Laminates.pdf
[4] Xavier Martinez, FrancescTuron & Fermin Otero “Homogenization procedure for the structural design of smart fuselage panels”, 8TH EASN-CEAS International workshop on manufacturing for growth and innovation, September 5TH, 2018, GLASGOW, UK
Document information
Published on 15/02/21
Accepted on 03/03/21
Submitted on 03/03/21
DOI: 10.23967/emus.2019.013
Licence: CC BY-NC-SA license
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