Tapia, Fidencio
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Preferred name
Tapia, Fidencio
Official Name
Tapia Rodríguez, Fidencio
Alternative Name
ftapia
Main Affiliation
ORCID
Scopus Author ID
57194045176
Researcher ID
T-2658-2018

Research Output

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Publication

New heuristics for assigning in the Multi-Depot Vehicle Routing Problem

2022 , Tapia, Fidencio , Acevedo, Hector

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Publication

EXPERIMENTAL STUDY OF ICE FORMATION ON AN AERONAUTICAL PITOT PROBE

2018 , Robert Jackel , Geydy Luz Gutierrez Urueta , Tapia, Fidencio , Juliana Braga Rodrigues Loureiro , Cintia Monreal Jimenez

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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 , Acevedo, Hector , Ch J. García , Emmanuel J. Gutierrez-Castañeda , Tapia, Fidencio

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Experimental Analysis of a 3-DOF Articulated Flat Empennage

2018 , Miguel Angel García-Terán , Ernesto Olguín-Díaz , Mauricio Gamboa-Marrufo , Angel Flores-Abad , Tapia, Fidencio

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Numerical and experimental characterisation of an aeronautic Pitot probe

2019 , R. Jäckel , G.L. Gutiérrez Urueta , Tapia, Fidencio , C. Monreal Jiménez

AbstractAeronautic 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.

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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 García , Tapia, Fidencio

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Design of an aeronautic pitot probe with a redundant heating system incorporating phase change materials

2020 , Robert Jäckel , Tapia, Fidencio , Geydy Gutiérrez-Urueta , Cintia Monreal Jiménez

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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-Contreras , Tapia, Fidencio

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A review on Pitot tube icing in aeronautics: Research- design and characterization – future trends

2021 , Robert Jäckel , Geydy Gutiérrez-Urueta , Tapia, Fidencio

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