Zobrazeno 1 - 9
of 9
pro vyhledávání: '"J. Calderon-Sanchez a"'
Publikováno v:
Engineering Applications of Computational Fluid Mechanics, Vol 15, Iss 1, Pp 865-888 (2021)
A dynamical system involving the decaying test of a partially filled liquid tank is analyzed in the present paper. This analysis is relevant for the design of aircraft fuel tanks, where the wings' structural dynamics are influenced by the complexity
Externí odkaz:
https://doaj.org/article/66e64fcdc9054fdea64c207027fcc85d
In Paper I of this series [Marrone, Colagrossi, Gonzalez,”A numerical study on the dissipation mechanisms in sloshing flows induced by violent and high frequency accelerations. Part I: Theoretical formulation and numerical investigation”], a theo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______2659::994bc8efdf04cf1373c244190f959435
https://zenodo.org/record/7760469
https://zenodo.org/record/7760469
Publikováno v:
Computers & Fluids. 183:16-27
The correct treatment of boundary conditions is a key step in the development of the SPH method. The SPH community has to face several challenges in this regard — in particular, a primordial aspect for any boundary formulation is to ensure the cons
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::08c1de1aa4956b3fc2403060936cb2be
https://doi.org/10.1016/j.compfluid.2019.02.020
https://doi.org/10.1016/j.compfluid.2019.02.020
Publikováno v:
Physical review. E. 103(5-1)
In this article, the classical Rayleigh-Taylor instability is extended to situations where the fluid is completely confined, in both the vertical and horizontal directions. This article starts with the two-dimensional (2D) viscous periodic case with
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::a4edea70f5cdddb7eb7ebf07dd56cf51
https://pubmed.ncbi.nlm.nih.gov/34134218
https://pubmed.ncbi.nlm.nih.gov/34134218
Publikováno v:
Physical review fluids (Online) 6 (2021). doi:10.1103/PhysRevFluids.6.114802
info:cnr-pdr/source/autori:Marrone S.; Colagrossi A.; Calderon-Sanchez J.; Martinez-Carrascal J./titolo:Numerical study on the dissipation mechanisms in sloshing flows induced by violent and high-frequency accelerations. II. Comparison against experimental data/doi:10.1103%2FPhysRevFluids.6.114802/rivista:Physical review fluids (Online)/anno:2021/pagina_da:/pagina_a:/intervallo_pagine:/volume:6
info:cnr-pdr/source/autori:Marrone S.; Colagrossi A.; Calderon-Sanchez J.; Martinez-Carrascal J./titolo:Numerical study on the dissipation mechanisms in sloshing flows induced by violent and high-frequency accelerations. II. Comparison against experimental data/doi:10.1103%2FPhysRevFluids.6.114802/rivista:Physical review fluids (Online)/anno:2021/pagina_da:/pagina_a:/intervallo_pagine:/volume:6
In Part I of this series [Marrone, Numerical study on the dissipation mechanisms in sloshing flows induced by violent and high-frequency accelerations. I. Theoretical formulation and numerical investigation, Phys. Rev. Fluids 6, 114801 (2021)10.1103/
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::3d68685f273b68dc380d4bd4af6e6eed
https://publications.cnr.it/doc/461793
https://publications.cnr.it/doc/461793
Publikováno v:
Proceedings of the 14th SPHERIC International Workshop | 14th SPHERIC International Workshop | June, 24-27 2019 | Exeter, UK
The wings of large civil passenger aircrafts, which are designed to withstand the loads occurring from atmospheric gusts and turbulence to landing impacts, still demand further research. This goal will be achieved through investigating the damping ef
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::de70cc62b4ca7b9e33809416dd9540eb
https://oa.upm.es/64529/
https://oa.upm.es/64529/
Publikováno v:
Ocean Engineering. 197:106823
This paper presents a parametric computer-based technique to build a B-spline model of a SWATH (Small Waterplane Area Twin Hull) ship hull. The method that is presented uses naval architecture parameters such as Displacement, Waterplane Area (Awp), C
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2882de91f156f0bd82e52bf40f2f7336
https://doi.org/10.1016/j.oceaneng.2019.106823
https://doi.org/10.1016/j.oceaneng.2019.106823
Autor:
Antonio Souto-Iglesias, J.L. Cercos-Pita, H. R. Diaz-Ojeda, J. Calderon-Sanchez, V. R. Bernal-Colio, Ricardo Abad
Publikováno v:
Volume 9: Offshore Geotechnics; Honoring Symposium for Professor Bernard Molin on Marine and Offshore Hydrodynamics.
The aim of this work is to approach the full design of an anti-roll tank through numerical simulation, looking for the way to minimize the computational cost. The results have been validated with experiments from a rectangular tank, a tank with a C-s
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d83def032ff632d92d9ac987401fbee7
https://doi.org/10.1115/omae2018-77609
https://doi.org/10.1115/omae2018-77609
Publikováno v:
Ocean Engineering. 103:144-152
A canonical wave impact problem is considered: the free fall of a rectangular block of a liquid, surrounded by a gas, which impacts on a flat floor. This problem calls for an explicit treatment of compressibility, which is directly responsible for th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e2d25ccf7f9abe3b575b886d208b4744
https://doi.org/10.1016/j.oceaneng.2015.04.060
https://doi.org/10.1016/j.oceaneng.2015.04.060