Tapia, Fidencio
Main Affiliation
Preferred name
Tapia, Fidencio
Official Name
Tapia Rodríguez, Fidencio
ORCID
0000-0002-5277-9568
Researcher ID
T-2658-2018
Scopus Author ID
57194045176
15 results
Now showing 1 - 10 of 15
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Item type:Publication, Improving the mechanical performance of 3D printed nylon through intelligent infill design(Springer Science and Business Media LLC, 2026-01-20) ;Reyna, Sandra L. Rodríguez ;Aguilera, Jorge H. Díaz; - Some of the metrics are blocked by yourconsent settings
Item type:Publication, Ensemble learning for mechanical behavior modeling of 3D-printed PLA under tension(Springer Science and Business Media LLC, 2026-02-09); ;Rodríguez-Reyna, S. L.; ;Acevedo-Parra, H. R.Díaz-Aguilera, J. H. - Some of the metrics are blocked by yourconsent settings
Item type:Publication, Optimization of the mechanical behavior of ABS and PLA 3D printed using heat treatments(Springer Science and Business Media LLC, 2025-03-17) ;S. L. Rodríguez-Reyna ;J. H. Díaz-Aguilera; ;Vladimir Escobar-Barrios - Some of the metrics are blocked by yourconsent settings
Item type:Publication, Design and optimization methodology for different 3D processed materials (PLA, ABS and carbon fiber reinforced nylon PA12) subjected to static and dynamic loads(2024) ;S.L. Rodríguez-Reyna ;J.H. Díaz-Aguilera; ;Ch J. GarcíaEmmanuel J. Gutierrez-CastañedaScopus© Citations 4 21 - Some of the metrics are blocked by yourconsent settings
Item type:Publication, A review on Pitot tube icing in aeronautics: Research- design and characterization – future trends(2021) ;Robert Jäckel ;Geydy Gutiérrez-UruetaScopus© Citations 19 15 1 - Some of the metrics are blocked by yourconsent settings
Item type:Publication, Synergistic effects of rubber-tire-powder and fluorogypsum in cement-based composite(2021) ;Sandra L. Rodríguez R. ;O. Domínguez ;Jorge H. Díaz A. ;Christian GarcíaScopus© Citations 11 32 1 - Some of the metrics are blocked by yourconsent settings
Item type:Publication, Evaluation of the mechanical behavior of fused deposition modeling (FDM)-printed virgin and recycled PLA parts using factorial design(2024) ;S. L. Rodríguez-Reyna ;J. H. Díaz-Aguilera ;J. P. García-ContrerasScopus© Citations 2 20 2 - Some of the metrics are blocked by yourconsent settings
Item type:Publication, Experimental Analysis of a 3-DOF Articulated Flat Empennage(2018) ;Miguel Angel García-Terán ;Ernesto Olguín-Díaz ;Mauricio Gamboa-Marrufo ;Angel Flores-Abad19 2 - Some of the metrics are blocked by yourconsent settings
Item type:Publication, 23 2 - Some of the metrics are blocked by yourconsent settings
Item type:Publication, Numerical and experimental characterisation of an aeronautic Pitot probe(2019) ;R. Jäckel ;G.L. Gutiérrez Urueta; C. Monreal Jiménez<jats:title>Abstract</jats:title><jats:p>Aeronautic Pitot probes (PPs) are extremely important for airspeed and altitude measurements in aviation. Failure of the instrument due to clogging caused by ice formation can lead to dangerous situations. In this work, a commercial aeronautic PP was characterised experimentally regarding its inner composition, material properties and its thermal performance in a climatic wind tunnel. Performance runs were taken out in order to analyse the thermal response of the PP under various operating conditions with a particular emphasis on the cooling process in the case of a heating element failure. Data for the thermal conductivity, diffusivity and specific heat for each material forming the PP were obtained. A numerical model to simulate the thermal behaviour of the PP was created using Comsol Multiphysics (CM). Experimental data were compared with their numerical counterparts for model validation purposes. After the model was validated, the operation of the PP in flight conditions was simulated. The failure of the conventional heating system was analysed to obtain the time until the PP reaches a tip temperature where ice formation can be expected. The tip temperature undercut the zero degrees Celsius mark 165 seconds after the heating element was switched off. The data collected in this work can be used to implement and validate mathematical models in order to predict the thermal performance of Pitot probes in flight conditions.</jats:p>Scopus© Citations 8 8 1
