Jiménez, MiguelCabrera, R.Armario, J.L.Graciani Díaz, EnriqueEstefani Morales, AlejandroMuñoz, KirsaGarcía, Eduardo HiguerasParís Carballo, Federico2021-03-092021-03-092021-01Jiménez, M., Cabrera, R., Armario, J.L., Graciani Díaz, E., Estefani Morales, A., Muñoz, K.,...,París Carballo, F. (2021). Development of a prototype test system for certification of curved fuselage panels. En 10th EASN International Conference on Innovation in Aviation and Space to the Satisfaction of the European Citizens, IOP Conference Series: Materials Science and Engineering, Vol. 1024, Issue 1,(012081), Virtual, Online: IOP Publishing Ltd.1757-8981https://hdl.handle.net/11441/105812Volume 1024, Issue 1 Article number 012081A prototype test system with capacity to reproduce combined loads representative of real loading cases of a curved fuselage panel has been developed. This prototype test system allows the structural validation of curved fuselage panels to be accomplished. The developed system is able to apply combined mechanical and pressurization loading states under quasi-static and dynamic loading conditions. It has been designed using CAD models and calculated with the aid of Finite Element models to ensure its integrity. A data acquisition system synchronized with a control system enables real time monitoring of test parameters.application/pdf8 p.engAttribution-NonCommercial-NoDerivatives 4.0 Internacionalhttp://creativecommons.org/licenses/by-nc-nd/4.0/Aircraft PropulsionFly by Wire ControlBlended-wing-body Configurationsinfo:eu-repo/semantics/conferenceObjectinfo:eu-repo/semantics/openAccesshttps://doi.org/10.1088/1757-899X/1024/1/012081