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Numerical analysis of n-octadecane melting process in a rectangular cell under reboosting maneuver conditions - imarina:9366511

Autor/es de la URV:Dubert, Diana Cristina / Gavaldà Martínez, Josefa / Masons Bosch, Jaime / Ruiz Plazas, Xavier / Simón Olmos, María José
Autor según el artículo:Dubert, D; Simón, MJ; Massons, J; Ruiz, X; Gavaldà, J
Direcció de correo del autor:xavier.ruiz@urv.cat
dianacristina.dubert@urv.cat
jaume.masons@urv.cat
fina.gavalda@urv.cat
mariajose.simon@urv.cat
Identificador del autor:0000-0002-7308-5872
0000-0003-4325-6084
0000-0001-7881-4192
0000-0002-4885-5935
Año de publicación de la revista:2024
Tipo de publicación:Journal Publications
Referencia de l'ítem segons les normes APA:Dubert, D; Simón, MJ; Massons, J; Ruiz, X; Gavaldà, J (2024). Numerical analysis of n-octadecane melting process in a rectangular cell under reboosting maneuver conditions. Acta Astronautica, 215(), 455-463. DOI: 10.1016/j.actaastro.2023.12.020
Referencia al articulo segun fuente origial:Acta Astronautica. 215 455-463
Resumen:The improvement of heat management based on Phase Change Materials (PCMs) is of increasing importance in space environments. In this context, a future ESA project called Effect of Marangoni Convection on heat transfer in Phase Change Materials (MarPCM) will evaluate the degree of improvement in heat transport using thermocapillarity as convective activator of the liquid phase generated during the melting. Since this type of project needs to be performed onboard International Space Station, ISS, it is of outmost importance to know if the accelerometric environment of the Station could affect the experiment results.To do so, various 2D simulations of the solid-liquid phase change were carried out using n-octadecane as PCM material, by considering a pre-selected acceleration signal coming from a real ISS reboosting maneuver (June 24, 2021). Different gravity scenarios have been considered by changing both the intensity and the orientation of the reboosting maneuver, parallel (x direction) and perpendicular (y direction) to the thermal gradients. The acceleration levels were enhanced up to 1000 times the intensity achieved during the real reboosting in order to predict the safety margins of the ISS experiment.The results showed alterations of the liquid-solid interface, during the melting process in the high g-level scenarios considered. In these cases, the oscillatory flow pattern became more complex detecting sudden changes in the main frequency which were maintained approximately 1000 s after the reboosting ended. Nevertheless, applying real boosting maneuver no significant influence in the melting process was detected.
DOI del artículo:10.1016/j.actaastro.2023.12.020
Enlace a la fuente original:https://www.sciencedirect.com/science/article/pii/S0094576523006501?via%3Dihub
Versión del articulo depositado:info:eu-repo/semantics/publishedVersion
Acceso a la licencia de uso:https://creativecommons.org/licenses/by/3.0/es/
Departamento:Química Física i Inorgànica
Enginyeria Mecànica
URL Documento de licencia:https://repositori.urv.cat/ca/proteccio-de-dades/
Áreas temáticas:Interdisciplinar
Geociências
Engineering, aerospace
Engenharias iv
Engenharias iii
Engenharias ii
Ciência da computação
Astronomia / física
Aerospace engineering & technology
Aerospace engineering
Palabras clave:Thermocapillary convection (marangoni effect)
Phase-change materials
Phase change materials
Openfoam software
Iss vibrational environment
Environment
Energy-storage
Accelerations
Entidad:Universitat Rovira i Virgili
Fecha de alta del registro:2024-08-03
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