Aeroelastic analysis using confocal sensors: experimental study and numerical validation with application to a future particle detector

Amatriain Carballo, Aitor ORCID: https://orcid.org/0000-0002-8024-9441, Angeletti, Massimo ORCID: https://orcid.org/0000-0002-8372-9125, Gargiulo, Corrado ORCID: https://orcid.org/0009-0001-4753-577X and Rubio Calzado, Gonzalo ORCID: https://orcid.org/0000-0002-6231-4801 (2024). Aeroelastic analysis using confocal sensors: experimental study and numerical validation with application to a future particle detector. "Aerospace Science and Technology", v. 151 ; ISSN 00341223. https://doi.org/10.1016/j.ast.2024.109313.

Descripción

Título: Aeroelastic analysis using confocal sensors: experimental study and numerical validation with application to a future particle detector
Autor/es:
Tipo de Documento: Artículo
Título de Revista/Publicación: Aerospace Science and Technology
Fecha: 1 Agosto 2024
ISSN: 00341223
Volumen: 151
Materias:
Palabras Clave Informales: Aeroelastic analysis; Air; air cooling; ALICE experiment; Budget Control; Confocal sensors; Cooling; Failure; Fluid structure interaction; Fluid-structure interaction; Fluid-structure interaction; Hadrons; Inner tracking system; Large Hadron Collider; Large-hadron colliders; Microstrip devices; Neutrons; Numerical Methods; Numerical validations; Particle Accelerators; Structural displacement; Vibration Analysis; Vibrations
Escuela: E.T.S. de Ingeniería Aeronáutica y del Espacio (UPM)
Departamento: Matemática Aplicada a la Ingeniería Aeroespacial
Licencias Creative Commons: Reconocimiento - Sin obra derivada - No comercial

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Resumen

This study investigates the structural displacements induced by aerodynamic loads in a future particle detector at the Large Hadron Collider (LHC): the Inner Tracking System 3 (ITS3) of the ALICE experiment. The development of an ultralight structure and use of air cooling lead to an unprecedentedly low material budget, resulting in improved accuracy compared to the current detector (ITS2). The airflow applied to the low -mass structure of the ITS3 is expected to cause vibrations, which requires an aeroelastic analysis that is performed using experimental and numerical methods. A novel experimental approach is proposed using confocal chromatic sensors to measure the structural displacements of an ITS3 prototype with submicron accuracy. A simplified mathematical model is developed for the fluid -structure interaction. The results obtained in the experimental setup show that the numerical model predicts the primary peaks in the spectrum of structural displacements induced by airflow. The validated model is used to analyze both the real anticipated configuration of the future ITS3 setup and potential modifications arising from changes in detector cooling and installation requirements.

Más información

ID de Registro: 86483
Identificador DC: https://oa.upm.es/86483/
Identificador OAI: oai:oa.upm.es:86483
URL Portal Científico: https://portalcientifico.upm.es/es/ipublic/item/10249069
Identificador DOI: 10.1016/j.ast.2024.109313
URL Oficial: https://www.sciencedirect.com/science/article/pii/...
Depositado por: iMarina Portal Científico
Depositado el: 22 Ene 2025 09:26
Ultima Modificación: 24 Ene 2025 10:12